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27 pages, 1989 KiB  
Article
A Safe and Efficient Global Path-Planning Method Considering Multiple Environmental Factors of the Moon Using a Distributed Computation Strategy
by Ruyan Zhou, Yuchuan Liu, Zhonghua Hong, Haiyan Pan, Yun Zhang, Yanling Han and Jiang Tao
Remote Sens. 2025, 17(5), 924; https://doi.org/10.3390/rs17050924 - 5 Mar 2025
Abstract
Lunar-rover path planning is a key topic in lunar exploration research, with safety and computational efficiency critical for achieving long-distance planning. This paper proposes a distributed path-planning method that considers multiple lunar environmental factors, addressing the issues of inadequate safety considerations and low [...] Read more.
Lunar-rover path planning is a key topic in lunar exploration research, with safety and computational efficiency critical for achieving long-distance planning. This paper proposes a distributed path-planning method that considers multiple lunar environmental factors, addressing the issues of inadequate safety considerations and low computational efficiency in current research. First, a set of safety evaluation rules is constructed by considering factors such as terrain slope, roughness, illumination, and rock abundance. Second, a distributed path-planning strategy based on a safety-map tile pyramid (DPPS-STP) is proposed, using a weighted A* algorithm with hash table-based open and closed lists (OC-WHT-A*) on a Spark cluster for efficient and safer path planning. Additionally, high-resolution digital orthophoto maps (DOM) are utilized for small crater detection, enabling more refined path planning built upon the overall mission-planning result. The method was validated in four lunar regions with distinct characteristics. The results show that DPPS-STP, which considers multiple environmental factors, effectively reduces the number of hazardous nodes and avoids crater obstacles. For long-distance tasks, it achieves an average speedup of up to 11.5 times compared to the single-machine OC-WHT-A*, significantly improving computational efficiency. Full article
(This article belongs to the Section Satellite Missions for Earth and Planetary Exploration)
20 pages, 4168 KiB  
Article
Development and Testing of a Novel Microstrip Photocathode ICCD for Lunar Remote Raman Detection
by Haiting Zhao, Xiangfeng Liu, Chao Chen, Weiming Xu, Jianan Xie, Zhenqiang Zhang, Ziqing Jiang, Xuesen Xu, Zhiping He, Rong Shu and Jianyu Wang
Sensors 2025, 25(5), 1528; https://doi.org/10.3390/s25051528 - 28 Feb 2025
Viewed by 257
Abstract
The intensified charge-coupled device (ICCD), known for its exceptional low-light detection performance and time-gating capability, has been widely applied in remote Raman spectroscopy systems. However, existing ICCDs face significant challenges in meeting the comprehensive requirements of high gating speed, high sensitivity, high resolution, [...] Read more.
The intensified charge-coupled device (ICCD), known for its exceptional low-light detection performance and time-gating capability, has been widely applied in remote Raman spectroscopy systems. However, existing ICCDs face significant challenges in meeting the comprehensive requirements of high gating speed, high sensitivity, high resolution, miniaturization, and adaptability to extreme environments for the upcoming lunar remote Raman spectroscopy missions. To address these challenges, this study developed a microstrip photocathode (MP-ICCD) specifically designed for lunar remote Raman spectroscopy. A comprehensive testing method was also proposed to evaluate critical performance parameters, including optical gating width, optimal gain voltage, and relative resolution. The MP-ICCD was integrated into a prototype remote Raman spectrometer equipped with a 40 mm aperture telescope and tested under outdoor sunlight conditions. The experimental results demonstrated that the developed MP-ICCD successfully achieved a minimum optical gating width of 6.0 ns and an optimal gain voltage of 870 V, with resolution meeting the requirements for Raman spectroscopy detection. Under outdoor solar illumination, the prototype remote Raman spectrometer utilizing the MP-ICCD accurately detected the Raman spectra of typical lunar minerals, including quartz, olivine, pyroxene, and plagioclase, at a distance of 1.5 m. This study provides essential technical support and experimental validation for the application of MP-ICCD in lunar Raman spectroscopy missions. Full article
(This article belongs to the Special Issue Advances in Raman Spectroscopic Sensing and Imaging)
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<p>Schematic diagram of MP-ICCD composition and working principle. (<b>a</b>) MP-ICCD “on” state. (<b>b</b>) MP-ICCD “off” state.</p>
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<p>(<b>a</b>) Model of microstrip photocathode image intensifier. (<b>b</b>) Equivalent distributed circuit of photocathode.</p>
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<p>(<b>a</b>) Physical object of microstrip photocathode image intensifier. (<b>b</b>) Physical object of integrated fluorescent screen fiber cone. (<b>c</b>) Front side of the coupled MP-ICCD. (<b>d</b>) Backside of the coupled MP-ICCD.</p>
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<p>Performance verification scheme for MP-ICCD.</p>
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<p>Test system and principles for OGRG-TS. (<b>a</b>) The physical setup of the test system; (<b>b</b>) the internal components of the test system; (<b>c</b>) the principle of minimum optical gate width testing; (<b>d</b>) the principle of optimal gain voltage testing; (<b>e</b>) timing diagram of optical gate testing. HVPS: high-voltage power supply, DDG: digital delay generator, EGW: electronic gate width, OGW: optical gate width.</p>
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<p>(<b>a</b>) ROI region with light input. (<b>b</b>) ROI region with no light input.</p>
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<p>(<b>a</b>) CCD spectral resolution measurement. (<b>b</b>) MP-ICCD spectral resolution measurement.</p>
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<p>Schematic diagram of TG-LRS. BM: beam expander, PD: photodetector, DM: dichroic mirror, LF: long-pass filter, CL: collection lens.</p>
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<p>(<b>a</b>) Pseudo-color pictures of the entire process of opening and closing the intensifier of MP-ICCD. (<b>b</b>) Minimum optical gate width.</p>
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<p>(<b>a</b>) Image showing the variation in fluorescent screen brightness with gain voltage under light input conditions. (<b>b</b>) Variation in fluorescent screen brightness with gain voltage under light input conditions. (<b>c</b>) Variation in fluorescent screen brightness with gain voltage under no light input conditions. (<b>d</b>) Variation in the SNR with gain voltage.</p>
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<p>(<b>a</b>) The 546.07 nm mercury–argon lamp spectrum acquired using CCD and MP-ICCD. (<b>b</b>) Comparison of CCD and MP-ICCD resolutions.</p>
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<p>(<b>a</b>) Raman spectrum of quartz. (<b>b</b>) Raman spectrum of olivine. (<b>c</b>) Raman spectrum of augite. (<b>d</b>) Raman spectrum of plagioclase.</p>
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23 pages, 4028 KiB  
Article
Development and Testing of a Compact Remote Time-Gated Raman Spectrometer for In Situ Lunar Exploration
by Haiting Zhao, Xiangfeng Liu, Weiming Xu, Daoyuantian Wen, Jianan Xie, Zhenqiang Zhang, Ziqing Jiang, Zongcheng Ling, Zhiping He, Rong Shu and Jianyu Wang
Remote Sens. 2025, 17(5), 860; https://doi.org/10.3390/rs17050860 - 28 Feb 2025
Viewed by 182
Abstract
Raman spectroscopy is capable of precisely identifying and analyzing the composition and properties of samples collected from the lunar surface, providing crucial data support for lunar scientific research. However, in situ Raman spectroscopy on the lunar surface faces challenges such as weak Raman [...] Read more.
Raman spectroscopy is capable of precisely identifying and analyzing the composition and properties of samples collected from the lunar surface, providing crucial data support for lunar scientific research. However, in situ Raman spectroscopy on the lunar surface faces challenges such as weak Raman scattering from targets, alongside requirements for lightweight and long-distance detection. To address these challenges, time-gated Raman spectroscopy (TG-LRS) based on a passively Q-switched pulsed laser and a linear intensified charge-coupled device (ICCD), which enable simultaneous signal amplification and background suppression, has been developed to evaluate the impact of key operational parameters on Raman signal detection and to explore miniaturization optimization. The TG-LRS system includes a 40 mm zoom telescope, a passively Q-switched 532 nm pulsed laser, a fiber optic delay line, a miniature spectrometer, and a linear ICCD detector. It achieves an electronic gating width under 20 ns. Within a detection range of 1.1–3.0 m, the optimal delay time varies linearly from 20 to 33 ns. Raman signal intensity increases with image intensifier gain, while the signal-to-noise ratio peaks at a gain range of 800–900 V before declining. Furthermore, the effects of focal depth, telescope aperture, laser energy, and integration time were studied. The Raman spectra of lunar minerals were successfully obtained in the lab, confirming the system’s ability to suppress solar background light. This demonstrates the feasibility of in situ Raman spectroscopy on the lunar surface and offers strong technical support for future missions. Full article
(This article belongs to the Special Issue Optical Remote Sensing Payloads, from Design to Flight Test)
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<p>Schematic of the principle of time-gated Raman spectroscopy detection.</p>
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<p>(<b>a</b>) TG-LRS working principle diagram. (<b>b</b>) TG-LRS physical diagram (<b>c</b>) TG-LRS internal component layout. (<b>d</b>) Indoor dark environment test. (<b>e</b>) Outdoor sunlight environment test.</p>
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<p>Lunar analog samples used to evaluate the capabilities of TG-LRS. (<b>a</b>) Augite. (<b>b</b>) Low-calcium pyroxene. (<b>c</b>) Olivine. (<b>d</b>) Plagioclase. (<b>e</b>) Quartz. (<b>f</b>) Apatite. (<b>g</b>) Gabbro. (<b>h</b>) Norite.</p>
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<p>Effect of gating width and delay time on Raman spectral signal intensity. (<b>a</b>) Signal intensity of quartz 461 cm<sup>−1</sup> Raman peak obtained by scanning with the parameters of a gating width of 10–20 ns and a delay time of 0–40 ns, (<b>b</b>) Raman spectrum of quartz measured at a distance of 1.5 m with a gating width of 20 ns and a delay time of 23 ns.</p>
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<p>(<b>a</b>) Quartz Raman signals at different detection distances versus laser echoes inside the instrument at a distance of 1.1 m. (<b>b</b>) Detection distance versus optimum delay time. (<b>c</b>,<b>d</b>) Variation of the quartz Raman signal with delay time from the laser echo inside the instrument at 1.1 m and 3.0 m detection distances, respectively.</p>
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<p>Effect of image intensifier gain on Raman signal intensity and SNR. (<b>a</b>,<b>b</b>) are the original spectra of the main Raman peaks of quartz and olivine at different gains, respectively. (<b>c</b>,<b>d</b>) are the relationships between the Raman signal and gain and the fitting equations for quartz and olivine, respectively. (<b>e</b>,<b>f</b>) are the Raman SNR versus gain for quartz and olivine, respectively.</p>
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<p>Effects of measurement parameters on Raman spectroscopy signals. (<b>a</b>) Variation of apatite Raman signal intensity with defocus amount, where negative values indicate movement towards the telescope and positive values indicate movement away from the telescope. (<b>b</b>) Changes in apatite Raman signal intensity with telescope aperture size, along with the corresponding changes in outgoing laser energy due to aperture obstruction. (<b>c</b>,<b>d</b>) show the relationship of apatite Raman signal intensity with laser energy and integration time at a fixed 40 mm clear aperture, respectively.</p>
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<p>Raman spectra of minerals collected at 1.5 m. (<b>a</b>) Raman spectrum of common augite. (<b>b</b>) Raman spectrum of low-calcium pyroxene. (<b>c</b>) Raman spectrum of olivine. (<b>d</b>) Raman spectrum of plagioclase. (<b>e</b>) Raman spectrum of quartz. (<b>f</b>) Raman spectrum of apatite. (<b>g</b>) Raman spectrum of gabbro. (<b>h</b>) Raman spectrum of norite.</p>
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<p>Signal intensity and signal-to-noise ratio of typical main mineral peaks at 1.5 m. (<b>a</b>) Intensity of the main peak of the Raman spectrum of the sample. (<b>b</b>) SNR of the main peak in the Raman spectrum of the sample.</p>
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<p>Effect of solar background light intensity and gating width on the Raman spectral SNR. (<b>a</b>) Variation of the SNR of the Raman peak at 461 cm<sup>−1</sup> in quartz. (<b>b</b>) Variation of the SNR of the Raman peak at 846 cm<sup>−1</sup> in olivine. (<b>c</b>) Variation of the SNR in the Raman spectrum of plagioclase at 507 cm<sup>−1</sup>.</p>
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22 pages, 5414 KiB  
Article
ARC-LIGHT: Algorithm for Robust Characterization of Lunar Surface Imaging for Ground Hazards and Trajectory
by Alexander Cushen, Ariana Bueno, Samuel Carrico, Corrydon Wettstein, Jaykumar Ishvarbhai Adalja, Mengxiang Shi, Naila Garcia, Yuliana Garcia, Mirko Gamba and Christopher Ruf
Aerospace 2025, 12(3), 177; https://doi.org/10.3390/aerospace12030177 - 24 Feb 2025
Viewed by 313
Abstract
Safe and reliable lunar landings are crucial for future exploration of the Moon. The regolith ejected by a lander’s rocket exhaust plume represents a significant obstacle in achieving this goal. It prevents spacecraft from reliably utilizing their navigation sensors to monitor their trajectory [...] Read more.
Safe and reliable lunar landings are crucial for future exploration of the Moon. The regolith ejected by a lander’s rocket exhaust plume represents a significant obstacle in achieving this goal. It prevents spacecraft from reliably utilizing their navigation sensors to monitor their trajectory and spot emerging surface hazards as they near the surface. As part of NASA’s 2024 Human Lander Challenge (HuLC), the team at the University of Michigan developed an innovative concept to help mitigate this issue. We developed and implemented a machine learning (ML)-based sensor fusion system, ARC-LIGHT, that integrates sensor data from the cameras, lidars, or radars that landers already carry but disable during the final landing phase. Using these data streams, ARC-LIGHT will remove erroneous signals and recover a useful detection of the surface features to then be used by the spacecraft to correct its descent profile. It also offers a layer of redundancy for other key sensors, like inertial measurement units. The feasibility of this technology was validated through development of a prototype algorithm, which was trained on data from a purpose-built testbed that simulates imaging through a dusty environment. Based on these findings, a development timeline, risk analysis, and budget for ARC-LIGHT to be deployed on a lunar landing was created. Full article
(This article belongs to the Special Issue Lunar, Planetary, and Small-Body Exploration)
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<p>General framework for sensor usage during EDL, showing navigation methodology at different stages, including deactivation for vertical descent.</p>
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<p>Prototype algorithm architecture; the blue box represents new data processing steps introduced by ARC-LIGHT between sensor readings and spacecraft GNC. Lidar and camera data are input. Image data is processed in initial CNN to determine optical depth of the image in multiple sectors and dehazed to improve signal-to-noise. Lidar data is filtered to remove significant outliers corresponding to strong PSI cloud backscatter. These intermediate quantities are combined in a second CNN to reconstruct the lidar scan without interference. Output is sent to GNC.</p>
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<p>Illustration of final descent where ARC-LIGHT is used to update spacecraft trajectory.</p>
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<p>Annotated image of SELENE. The tank is sealed with latches, allowing for the lid to be removed for interior access.</p>
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<p>(<b>a</b>) Dimensionless scattering coefficients for irregular regolith grains (dashed) and spherical DEHS droplets (solid) of different radii. (<b>b</b>) Scattering phase function, normalized to the single scattering albedo, of the same size particles for 0.65 μm wavelength light. Regolith data from [<a href="#B40-aerospace-12-00177" class="html-bibr">40</a>].</p>
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<p>At the top are the example camera images with their respective lidar scans below them from SELENE. DEHS density increases from (left) to (right) panels. The lidar scan crosses the center of the image from top to bottom.</p>
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<p>Prototype CNN architecture. The training images with known optical depths are used to train the network, which is composed of multiple layers of n neurons each. For a given image (100 × 100 pixel values), it outputs an estimate of the optical depth (value between 0 and 1).</p>
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<p>CNN training metrics. (<b>a</b>) CNN estimate of the optical depth for the test data, plotted against the true value before training. (<b>b</b>) CNN estimate of the optical depth for the test data, plotted against the true value after training completes. (<b>c</b>) Plot of CNN loss across the training epochs.</p>
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<p>(<b>a</b>) Lidar distance attenuation as a function of angle. 0 degrees is looking straight down. Color represents the optical depth of the tank for each scan, ranging from 0 (red) to 0.6 (blue). Solid lines are lidar data; dotted lines are analytic fit. (<b>b</b>) Plot of Equation (3) free parameters as a function of τ.</p>
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<p>Projections of lidar scans for three DEHS densities. On the left side are the images from SELENE labeled by the measured optical depth (τ) and CNN estimate (<math display="inline"><semantics> <mrow> <mover accent="true"> <mrow> <mi>τ</mi> </mrow> <mo>^</mo> </mover> </mrow> </semantics></math>). On the right side are their respective lidar scan, showing the raw lidar scan (dashed blue), ground truth geometry (black solid), and projected lidar scan using <math display="inline"><semantics> <mrow> <mover accent="true"> <mrow> <mi>τ</mi> </mrow> <mo>^</mo> </mover> </mrow> </semantics></math> (blue solid).</p>
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<p>Timeline organized by milestones, year, and month.</p>
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<p>Budget estimating the total cost of the development of ARC-LIGHT.</p>
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19 pages, 8277 KiB  
Article
Physics-Based Noise Modeling and Deep Learning for Denoising Permanently Shadowed Lunar Images
by Haiyan Pan, Binbin Chen and Ruyan Zhou
Appl. Sci. 2025, 15(5), 2358; https://doi.org/10.3390/app15052358 - 22 Feb 2025
Viewed by 313
Abstract
The Narrow-Angle Cameras (NACs) onboard the Lunar Reconnaissance Orbiter Camera (LROC) capture lunar images that play a crucial role in current lunar exploration missions. Among these images, those of the Moon’s permanently shadowed regions (PSRs) are highly noisy, obscuring the lunar topographic features [...] Read more.
The Narrow-Angle Cameras (NACs) onboard the Lunar Reconnaissance Orbiter Camera (LROC) capture lunar images that play a crucial role in current lunar exploration missions. Among these images, those of the Moon’s permanently shadowed regions (PSRs) are highly noisy, obscuring the lunar topographic features within these areas. While significant advancements have been made in denoising techniques based on deep learning, the direct acquisition of paired clean and noisy images from the PSRs of the Moon is costly, making dataset acquisition expensive and hindering network training. To address this issue, we employ a physical noise model based on the imaging principles of the LROC NACs to generate noisy pairs of images for the Moon’s PSRs, simulating realistic lunar imagery. Furthermore, inspired by the ideas of full-scale skip connections and self-attention models (Transformers), we propose a denoising method based on deep information convolutional neural networks. Using a dataset synthesized through the physical noise model, we conduct a comparative analysis between the proposed method and existing state-of-the-art denoising approaches. The experimental results demonstrate that the proposed method can effectively recover topographic features obscured by noise, achieving the highest quantitative metrics and superior visual results. Full article
(This article belongs to the Section Applied Physics General)
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<p>The flowchart of data synthesis.</p>
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<p>Compression function.</p>
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<p>Original image selection.</p>
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<p>Illustration of simulated images. (<b>a</b>) Noiseless images with sufficient lighting; (<b>b</b>) Synthesized noisy images.</p>
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<p>Real images of PSRs.</p>
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<p>The structure of the FRET.</p>
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<p>The structure of the REWin block.</p>
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<p>The structure of the SW-MSA.</p>
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<p>The structure of the GFRN.</p>
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<p>The structure of the GCEN.</p>
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<p>Denoising results of the simulated images. (<b>a</b>) Latitude: −72.78° Longitude: 310.81° (<b>b</b>) Latitude: 57.36° Longitude: 194.01° (<b>c</b>) Latitude: −58.12° Longitude: 153.74° (<b>d</b>) Latitude: −32.57° Longitude: 153.23°.</p>
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<p>Denoising result of the real images. (<b>a</b>) Latitude: −88.13° Longitude: 216.34° (<b>b</b>) Latitude: −70.26° Longitude: 187.91° (<b>c</b>) Latitude: −83.63° Longitude: 16.12° (<b>d</b>) Latitude: −83.52° Longitude: 56.23°.</p>
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16 pages, 4878 KiB  
Technical Note
A Robust Digital Elevation Model-Based Registration Method for Mini-RF/Mini-SAR Images
by Zihan Xu, Fei Zhao, Pingping Lu, Yao Gao, Tingyu Meng, Yanan Dang, Mofei Li and Robert Wang
Remote Sens. 2025, 17(4), 613; https://doi.org/10.3390/rs17040613 - 11 Feb 2025
Viewed by 352
Abstract
SAR data from the lunar spaceborne Reconnaissance Orbiter’s (LRO) Mini-RF and Chandrayaan-1’s Mini-SAR provide valuable insights into the properties of the lunar surface. However, public lunar SAR data products are not properly registered and are limited by localization issues. Existing registration methods for [...] Read more.
SAR data from the lunar spaceborne Reconnaissance Orbiter’s (LRO) Mini-RF and Chandrayaan-1’s Mini-SAR provide valuable insights into the properties of the lunar surface. However, public lunar SAR data products are not properly registered and are limited by localization issues. Existing registration methods for Earth SAR have proven to be inadequate in their robustness for lunar data registration. And current research on methods for lunar SAR has not yet focused on producing globally registered datasets. To solve these problems, this article introduces a robust automatic registration method tailored for S-band Level-1 Mini-RF and Mini-SAR data with the assistance of lunar DEM. A simulated SAR image based on real lunar DEM data is first generated to assist the registration work, and then an offset calculation approach based on normalized cross-correlation (NCC) and specific processing, including background removal, is proposed to achieve the registration between the simulated image, and the real image. When applying Mini-RF images and Mini-SAR images, high robustness and good accuracy are exhibited, which produces fully registered datasets. After processing using the proposed method, the average error between Mini-RF images and DEM references was reduced from approximately 3000 m to about 100 m. To further explore the additional improvement of the proposed method, the registered lunar SAR datasets are used for further analysis, including a review of the circular polarization ratio (CPR) characteristics of anomalous craters. Full article
(This article belongs to the Section Engineering Remote Sensing)
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<p>Flowchart of the proposed registration method and examples of OC image simulation/registration results. The left part shows the example of generating simulated OC images from local incidence angle images. The right part shows an example of correcting the offset in Level-1 SAR images.</p>
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<p>Example of real SAR images and simulated images before eliminating background and after eliminating background, with the correlation coefficient comparison.</p>
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<p>Mini-RF data registration results of the proposed method and GAMMA’s correlation and feature extraction methods, shown by fusion images of real Level-1 SAR and simulated images.</p>
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<p>Distribution of standard craters in lunar South Pole and examples of standard craters in Mini-RF (<b>a1</b>,<b>b1</b>,<b>c1</b>) and DEM hillshade images (<b>a2</b>,<b>b2</b>,<b>c2</b>).</p>
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<p>Scatter plot of distance error (m); each point represents a crater target and its distance error. And separate histogram of distance error distribution in x/y direction of &lt;10 km (in blue) and &gt;10 km (in orange) targets.</p>
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<p>Normalized density scatterplot showing the relationship of offsets/distance errors in the SAR-image domain and operation time of Mini-SAR (<b>a</b>) and Mini-RF (<b>b</b>). ①②/①②③④ represent the concentrated distribution and variation trend of the offsets.</p>
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<p>Scatter plot of average ΔCPR in South Pole crater interior/exterior areas in the Mini-RF west-looking mosaic. The craters with a diameter &lt;8 km were not included in Fa’s research. Craters with ΔCPR &gt; 0.1 were identified as anomalous craters.</p>
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<p>The mismatching cases of Mini-RF data (excerpt from lsz_04472_1cd_xku_74n234_v1 and lsz_04866_1cd _xku_87n047_v1).</p>
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20 pages, 2953 KiB  
Article
Regolith-Rich PEEK Composite Bricks: Steps Towards Space-Ready Lunar Construction Materials
by Roberto Torre, Carlo Giovanni Ferro, Lorenzo Bono and Aidan Cowley
Appl. Sci. 2025, 15(2), 679; https://doi.org/10.3390/app15020679 - 11 Jan 2025
Viewed by 668
Abstract
This study introduces a novel composite construction material composed of lunar regolith combined with PEEK in dry powder form. The work demonstrates significant advantages over alternative methods, primarily by reducing production power consumption and simplifying the manufacturing process. Building on previous research that [...] Read more.
This study introduces a novel composite construction material composed of lunar regolith combined with PEEK in dry powder form. The work demonstrates significant advantages over alternative methods, primarily by reducing production power consumption and simplifying the manufacturing process. Building on previous research that explored binder optimization through process simplification and targeting predefined shapes, this work delves deeper into a comparative analysis of high-performance thermoplastics. Among the various options, PEEK demonstrates the most favorable properties. The study investigates key processing parameters and evaluates the effects of vacuum processing and temperature testing on mechanical properties. The research also evaluates the effects of vacuum processing and temperature testing to assess the material’s performance under lunar conditions. Comparative analysis is performed with standard performance of various reinforced and unreinforced concretes and with standard requirements for construction bricks as per ASTM standards. This shows that the composite, with an organic binder content as low as 5 wt%, has great potential. Notably, the improvements achieved through vacuum curing ensure compliance with lunar environmental conditions and alignment with most Earth-based engineering standards. Samples compacted at 7.50 MPa with 10 wt% binder, and tested at room temperature, achieve a compression strength of 16.3 MPa, exceeding that of industrial floor bricks and matching that of building bricks used on Earth. Bending strength (7.4 MPa) aligns with steel fiber-reinforced and high-strength concretes. Vacuum curing further enhances these properties, with an observed increase of +66% in bending strength and +33% in compression strength. Full article
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<p>Proof-of-concept designs for interlocking elements made from regolith-rich composite material, demonstrating the feasibility of constructing modular, mortar-free structures using minimal thermoplastic binders.</p>
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<p>Manufacturing steps for PEEK- and PLA-based samples: The blue boxes indicate the process parameters specific to PLA, highlighting where they differ from those used for PEEK.</p>
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<p>Example of reference bending and compression specimens used throughout the experimental campaign. The geometries shown are representative of all specimens, which were ideally identical and used for both air-cured and vacuum-cured samples.</p>
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<p>Experimental results: bending strength and modulus per DoE run.</p>
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<p>Experimental results: compression strength and modulus per DoE run.</p>
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<p>Bending strength and modulus: main effects plots for means.</p>
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<p>Compression strength and modulus: main effects plots for means.</p>
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<p>Summary of experimental results for the vacuum-processed samples: bending strength/modulus at different conditioning temperatures.</p>
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<p>Summary of experimental results for the vacuum-processed samples: compression strength/modulus at different conditioning temperatures.</p>
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<p>Bending strength: Comparison of the requirements for three grades of steel fiber-reinforced concrete [<a href="#B26-applsci-15-00679" class="html-bibr">26</a>] against experimental data. The black dots show the bending strengths of DoE samples (cured in air, tested at +20 °C); the additional points associated with run 8 (same compaction pressure and binder percentage) represent samples cured in vacuum and tested at various temperatures.</p>
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<p>Compression strength: comparison of the requirements for different brick applications [<a href="#B18-applsci-15-00679" class="html-bibr">18</a>,<a href="#B19-applsci-15-00679" class="html-bibr">19</a>,<a href="#B20-applsci-15-00679" class="html-bibr">20</a>,<a href="#B63-applsci-15-00679" class="html-bibr">63</a>] against experimental data. The black dots show the bending strengths of DoE samples (cured in air, tested at +20 °C); the additional points associated with run 8 (same compaction pressure and binder percentage) represent samples cured in vacuum and tested at various temperatures.</p>
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9 pages, 963 KiB  
Article
Reconcentrating the Ionic Liquid EMIM-HSO4 Using Direct Contact Membrane Distillation
by Mark J. Wong, Viral Sagar and Joan G. Lynam
Molecules 2025, 30(2), 211; https://doi.org/10.3390/molecules30020211 - 7 Jan 2025
Viewed by 383
Abstract
Adequate water supplies are crucial for missions to the Moon, since water is essential for astronauts’ health. Ionic liquids (ILs) have been investigated for processing metal oxides, the main components of lunar regolith, to separate oxygen and metals. The IL must be diluted [...] Read more.
Adequate water supplies are crucial for missions to the Moon, since water is essential for astronauts’ health. Ionic liquids (ILs) have been investigated for processing metal oxides, the main components of lunar regolith, to separate oxygen and metals. The IL must be diluted in the process. Recycling this diluted IL post-processing is important to reduce the materials required in resupply missions. In addition, water will be needed in lunar greenhouses for growing food and aiding in sustaining a habitable environment. Direct contact membrane distillation (DCMD) is a new technology for water purification that was examined in this study for its feasibility to concentrate IL. Hydrophobic membranes composed of polytetrafluoroethylene (PTFE) and polyvinylidene (PVDF) were found to hold promise in separating solutes from water to concentrate a diluted IL solution and to recover water. A bench-scale DCMD system was employed to test this method at temperatures of 50 °C, 65 °C, and 80 °C. Hence, the benefits and limitations of DCMD with PTFE and PVDF membranes were explored for the aqueous IL 1-ethyl-3 methylimidazolium hydrogen sulfate for DCMD performed at different temperatures. Full article
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<p>Calibration curve to establish the relationship between the conductivity and mass percentage of ionic liquid (IL).</p>
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<p>Calibration curve to establish the relationship between mass percentage of IL and light absorption.</p>
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<p>A calibration curve for the absorbance of light at 265 nm for different mass percentages of IL.</p>
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<p>The effect of DCMD temperature on the change in concentration of the IL solution.</p>
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25 pages, 13675 KiB  
Article
KANDiff: Kolmogorov–Arnold Network and Diffusion Model-Based Network for Hyperspectral and Multispectral Image Fusion
by Wei Li, Lu Li, Man Peng and Ran Tao
Remote Sens. 2025, 17(1), 145; https://doi.org/10.3390/rs17010145 - 3 Jan 2025
Viewed by 534
Abstract
In recent years, the fusion of hyperspectral and multispectral images in remote sensing image processing still faces challenges, primarily due to their complexity and multimodal characteristics. Diffusion models, known for their stable training process and exceptional image generation capabilities, have shown good application [...] Read more.
In recent years, the fusion of hyperspectral and multispectral images in remote sensing image processing still faces challenges, primarily due to their complexity and multimodal characteristics. Diffusion models, known for their stable training process and exceptional image generation capabilities, have shown good application potential in this field. However, when dealing with multimodal data, it may prove challenging for the models to fully capture the intricate relationships between the modalities, which may result in incomplete information integration and a small amount of remaining noise in the generated images. To address these problems, we propose a new model, KanDiff, for hyperspectral and multispectral image fusion. To address the differences in modal information between multispectral and hyperspectral images, KANDiff incorporates Kolmogorov–Arnold Networks (KAN) to guide the inputs. It helps the model understand the complex relationships between the modalities by replacing the fixed activation function in the traditional MLP with a learnable activation function. Furthermore, the image generated by the diffusion model may exhibit a small amount of the remaining noise. Convolutional Neural Networks (CNNs) effectively extract local features through their convolutional layers and achieve noise suppression via layer-by-layer feature representation. Therefore, the MergeCNN module is further introduced to enhance the fusion effect, resulting in smoother and more accurate outcomes. Experimental results on the public CAVE and Harvard datasets indicate that KanDiff has achieved improvements over current high-performance methods across several metrics, particularly showing significant enhancements in the peak signal-to-noise ratio (PSNR) and the structural similarity index measure (SSIM), thus demonstrating superior performance. Additionally, we have created an image fusion dataset of the lunar surface, and KANDiff exhibits robust performance on this dataset as well. This work introduces an effective solution for addressing the challenges posed by missing high-resolution hyperspectral images (HRHS) data, which is essential for tasks including landing site selection and resource exploration within the realm of deep space exploration. Full article
(This article belongs to the Section Remote Sensing Image Processing)
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<p>The forward diffusion process and the backward process (<b>a</b>) of the diffusion model (<b>b</b>).</p>
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<p>KANDiff flowchart: The difference between HSI_GT and HSI_UP (RES) is used as the input of the diffusion model. MSI and HSI_UP are first fused through wavelet transform as the condition of the diffusion model. The KAN module is used as a guide. The output of the diffusion model is added to HSI_UP to obtain HSI_D. Finally, HSI_D and MSI are concatenated and input to the MergeCNN module. (<b>a</b>) The KAN-based guidance module. (<b>b</b>) The diffusion module. (<b>c</b>) The MergeCNN module.</p>
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<p>The details of the diffusion module: (<b>a</b>) depicts the structure of the encoder, middle layers, and decoder, and (<b>b</b>) depicts the structure of the block. ‘cond’ represents the condition of the diffusion model, ‘res’ is the difference between HSI_GT and HSI_UP, and ‘SiLu’ is an activation function.</p>
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<p>Test images from the CAVE dataset. (<b>a</b>) <span class="html-italic">Balloons</span>. (<b>b</b>) <span class="html-italic">Flowers</span>. (<b>c</b>) <span class="html-italic">Chart and stuffed toy</span>. (<b>d</b>) <span class="html-italic">Clay</span>. (<b>e</b>) <span class="html-italic">Fake and real beers</span>. (<b>f</b>) <span class="html-italic">Jelly beans</span>. (<b>g</b>) <span class="html-italic">Fake and real lemon slices</span>. (<b>h</b>) <span class="html-italic">Fake and real tomatoes</span>. (<b>i</b>) <span class="html-italic">Feathers</span>. (<b>j</b>) <span class="html-italic">Hairs</span>. (<b>k</b>) <span class="html-italic">compact disc (CD)</span>.</p>
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<p>Test images from the Harvard dataset. (<b>a</b>) <span class="html-italic">Tree</span>. (<b>b</b>) <span class="html-italic">Door</span>. (<b>c</b>) <span class="html-italic">Window</span>. (<b>d</b>) <span class="html-italic">Backpack</span>. (<b>e</b>) <span class="html-italic">Bikes</span>. (<b>f</b>) <span class="html-italic">Wall</span>. (<b>g</b>) <span class="html-italic">Sofa1</span>. (<b>h</b>) <span class="html-italic">Fence</span>. (<b>i</b>) <span class="html-italic">Sofa2</span>. (<b>j</b>) <span class="html-italic">Parcels</span>.</p>
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<p>Test images from the Moon dataset.</p>
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<p>The first and third rows of the four-row legend show the GT of “Feathers” in the CAVE dataset and the true colour representation of the fusion results for the KANDiff and 10 compared methods, respectively. The second and fourth rows show the residuals between the fusion results of the different methods and GT. (<b>a</b>) GT. (<b>b</b>) KANDiff. (<b>c</b>) PSRT. (<b>d</b>) DRPNN. (<b>e</b>) MOG-DCN. (<b>f</b>) DICNN. (<b>g</b>) DDIF. (<b>h</b>) FisionNet. (<b>i</b>) MSDCNN. (<b>j</b>) PNN. (<b>k</b>) PanNet. (<b>l</b>) BDSD.</p>
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<p>Spectral vectors of the GT and the benchmark.</p>
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<p>The first and third rows of the four-row legend show the GT of a test image from the Harvard dataset and the true color representation of the fusion results for the 10 comparison methods and KANDiff, respectively. The second and fourth rows show the residuals between the fusion results of the various methods and GT. (<b>a</b>) GT. (<b>b</b>) KANDiff. (<b>c</b>) PSRT. (<b>d</b>) DRPNN. (<b>e</b>) MOG-DCN. (<b>f</b>) DICNN. (<b>g</b>) DDIF. (<b>h</b>) FisionNet. (<b>i</b>) MSDCNN. (<b>j</b>) PNN. (<b>k</b>) PanNet. (<b>l</b>) BDSD.</p>
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<p>The first and third rows of the four-row legend show the GT of a test image from the Moon dataset and the true color representation of the fusion results for the 10 comparison methods and KANDiff, respectively. The second and fourth rows show the residuals between the fusion results of the various methods and GT. (<b>a</b>) GT. (<b>b</b>) KANDiff. (<b>c</b>) PSRT. (<b>d</b>) DRPNN. (<b>e</b>) MOG-DCN. (<b>f</b>) DICNN. (<b>g</b>) DDIF. (<b>h</b>) FisionNet. (<b>i</b>) MSDCNN. (<b>j</b>) PNN. (<b>k</b>) PanNet. (<b>l</b>) BDSD.</p>
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26 pages, 12157 KiB  
Article
A Machine Learning Approach for the Autonomous Identification of Hardness in Extraterrestrial Rocks from Digital Images
by Shuyun Liu, Haifeng Zhao, Zihao Yuan, Liping Xiao, Chengcheng Shen, Xue Wan, Xuhai Tang and Lu Zhang
Aerospace 2025, 12(1), 26; https://doi.org/10.3390/aerospace12010026 - 31 Dec 2024
Viewed by 470
Abstract
Understanding rock hardness on extraterrestrial planets offers valuable insights into planetary geological evolution. Rock hardness correlates with morphological parameters, which can be extracted from navigation images, bypassing the time and cost of rock sampling and return. This research proposes a machine-learning approach to [...] Read more.
Understanding rock hardness on extraterrestrial planets offers valuable insights into planetary geological evolution. Rock hardness correlates with morphological parameters, which can be extracted from navigation images, bypassing the time and cost of rock sampling and return. This research proposes a machine-learning approach to predict extraterrestrial rock hardness using morphological features. A custom dataset of 1496 rock images, including granite, limestone, basalt, and sandstone, was created. Ten features, such as roundness, elongation, convexity, and Lab color values, were extracted for prediction. A foundational model combining Random Forest (RF) and Support Vector Regression (SVR) was trained through cross-validation. The output of this model was used as the input for a meta-model, undergoing linear fitting to predict Mohs hardness, forming the Meta-Random Forest and Support Vector Regression (MRFSVR) model. The model achieved an R2 of 0.8219, an MSE of 0.2514, and a mean absolute error of 0.2431 during validation. Meteorite samples were used to validate the MRFSVR model’s predictions. The model is used to predict the hardness distribution of extraterrestrial rocks using images from the Tianwen-1 Mars Rover Navigation and Terrain Camera (NaTeCam) and a simulated lunar rock dataset from an open-source website. The results demonstrate the method’s potential for enhancing extraterrestrial exploration. Full article
(This article belongs to the Special Issue Aerospace Technology and Space Informatics)
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<p>Conceptual diagram of the working scenario of this paper.</p>
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<p>Flow chart of MRFSVR.</p>
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<p>Flowchart of k-fold cross-validation.</p>
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<p>Schematic diagram of the principle of SVR.</p>
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<p>Schematic diagram of the principle of RF.</p>
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<p>Example of the original rock dataset created for this study (grid scale: 1 cm): (<b>a1</b>–<b>a3</b>) Granite; (<b>b1</b>–<b>b3</b>) Rhyolite; (<b>c1</b>–<b>c3</b>) Basalt; (<b>d1</b>–<b>d3</b>) Sandstone; (<b>e1</b>–<b>e3</b>) Limestone.</p>
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<p>Example of the original rock dataset created for this study (grid scale: 1 cm): (<b>a1</b>–<b>a3</b>) Granite; (<b>b1</b>–<b>b3</b>) Rhyolite; (<b>c1</b>–<b>c3</b>) Basalt; (<b>d1</b>–<b>d3</b>) Sandstone; (<b>e1</b>–<b>e3</b>) Limestone.</p>
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<p>(<b>a</b>) Rock RGB image; (<b>b</b>) Edge detection graph; (<b>c</b>) Denoising results.</p>
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<p>(<b>a</b>) Illustration of the minimal circumscribed circle; (<b>b</b>) The smallest circumscribed circle generated.</p>
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<p>Illustration of rocks and its corresponding minimum enclosing rectangle.</p>
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<p>Schematic diagram of the GLCM.</p>
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<p>Feature distribution plots for five types of rocks: (<b>a</b>) Lab mean value; (<b>b</b>) Radius; (<b>c</b>) Contrast; (<b>d</b>) Correlation; (<b>e</b>) Energy; (<b>f</b>) Homogeneity; (<b>g</b>) Fractal dimension; (<b>h</b>) Ovality; (<b>i</b>) Extension; (<b>j</b>) Convex.</p>
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<p>The mean distribution of nine characteristic values.</p>
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<p>The mean distribution of Lab mean values.</p>
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<p>Dataset heatmap.</p>
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<p>The evaluation parameter results.</p>
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<p>Residual analysis results for the four models.</p>
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<p>Comparison of prediction results.</p>
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<p>The meteorites used in the experiment: (<b>a</b>) KERIYA001 meteorite #1; (<b>b</b>) KERIYA001 meteorite #2; (<b>c</b>) unknown meteorite specimen #3; (<b>d</b>) unknown meteorite specimen #4; (<b>e</b>) unknown meteorite specimen #5.</p>
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<p>Distribution of predicted values for meteorites.</p>
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<p>(<b>a</b>) Navigation image of Tianwen-1; (<b>b</b>) Image segmented by U-NET; (<b>c</b>) Binary image after image processing; (<b>d</b>) Visualization of segmentation results.</p>
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<p>(<b>a</b>) Original image; (<b>b</b>) Binary image; (<b>c</b>) Single rock RGB image; (<b>d</b>) Single rock binary image; (<b>e</b>) Hardness prediction on the Martian surface.</p>
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<p>(<b>a</b>) Lunar original image; (<b>b</b>) Lunar binary image; (<b>c</b>) Single rock RGB image; (<b>d</b>) Single rock binary image; (<b>e</b>) Hardness prediction on the lunar surface.</p>
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23 pages, 7175 KiB  
Article
Integrated Analysis of Water Ice Detection in Erlanger Crater, Lunar North Pole: Insights from Chandrayaan-1 Mini-SAR and Chandrayaan-2 DFSAR Data
by Chandani Sahu, Shashi Kumar, Himanshu Govil and Shovan Lal Chattoraj
Remote Sens. 2025, 17(1), 31; https://doi.org/10.3390/rs17010031 - 26 Dec 2024
Viewed by 595
Abstract
The characterization of the lunar surface and subsurface through the utilization of synthetic aperture radar data has assumed a pivotal role in the domain of lunar exploration science. This investigation concentrated on the polarimetric analysis aimed at identifying water ice within a specific [...] Read more.
The characterization of the lunar surface and subsurface through the utilization of synthetic aperture radar data has assumed a pivotal role in the domain of lunar exploration science. This investigation concentrated on the polarimetric analysis aimed at identifying water ice within a specific crater, designated Erlanger, located at the lunar north pole, which is fundamentally a region that is perpetually shaded from solar illumination. The area that is perpetually shaded on the moon is defined as that region that is never exposed to sunlight due to the moon’s slightly tilted rotational axis. These permanently shaded regions serve as cold traps for water molecules. To ascertain the presence of water ice within the designated study area, we conducted an analysis of two datasets from the Chandrayaan mission: Mini-SAR data from Chandrayaan-1 and Dual-Frequency Synthetic Aperture Radar (DFSAR) data from Chandrayaan-2. The polarimetric analysis of the Erlanger Crater, located in a permanently shadowed region of the lunar north pole, utilizes data from the Dual-Frequency Synthetic Aperture Radar (DFSAR) and the Mini-SAR. This study focuses exclusively on the L-band DFSAR data due to the unavailability of S-band data for the Erlanger Crater. The crater, identified by the PSR ID NP_869610_0287570, is of particular interest for its potential water ice deposits. The analysis employs three decomposition models—m-delta, m-chi, and m-alpha—derived from the Mini-SAR data, along with the H-A-Alpha model known as an Eigenvector and Eigenvalue model, applied to the DFSAR data. The H-A-Alpha helps in assessing the entropy and anisotropy of the lunar surface. The results reveal a correlation between the hybrid polarimetric models (m-delta, m-chi, and m-alpha) and fully polarimetric parameters (entropy, anisotropy, and alpha), suggesting that volume scattering predominates inside the crater walls, while surface and double bounce scattering are more prevalent in the right side of the crater wall and surrounding areas. Additionally, the analysis of the circular polarization ratio (CPR) from both datasets suggests the presence of water ice within and around the crater, as values greater than 1 were observed. This finding aligns with other studies indicating that the high CPR values are indicative of ice deposits in the lunar polar regions. The polarimetric analysis of the Erlanger Crater contributes to the understanding of lunar polar regions and highlights the potential for future exploration and resource utilization on the Moon. Full article
(This article belongs to the Special Issue New Approaches in High-Resolution SAR Imaging)
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<p>L-band color composite DFSAR for the north pole of the lunar surface with the PSR id of Erlanger. Clementine image is used as base map to show the north pole of lunar surface.</p>
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<p>Detailed methodology flow diagram.</p>
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<p>m-delta (δ) decomposition of Mini-SAR data Chandrayaan-1: (<b>a</b>) surface scattering; and (<b>b</b>) double bounce scattering.</p>
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<p>m-delta (δ) decomposition of Mini-SAR data Chandrayaan-1: (<b>a</b>) volumetric Scattering; and (<b>b</b>) RGB composite image, where G stands for volumetric, R for double bounce, and B for surface scattering.</p>
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<p>m-chi (χ) decomposition of Mini-SAR data Chandrayaan-1: (<b>a</b>) surface Scattering; and (<b>b</b>) double bounce scattering.</p>
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<p>m-chi (χ) decomposition of Mini-SAR data Chandrayaan-1: (<b>a</b>) volumetric Scattering; and (<b>b</b>) RGB composite image, where G stands for volumetric, R for double bounce, and B for surface scattering.</p>
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<p>m-alpha (α) decomposition of Mini-SAR data Chandrayaan-1: (<b>a</b>) surface scattering; and (<b>b</b>) double bounce scattering.</p>
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<p>m-alpha decomposition of Chandrayaan-1 Mini-SAR data: (<b>a</b>) volumetric scattering; and (<b>b</b>) RGB composite where G stands for volumetric, R for double bounce, and B for surface scattering.</p>
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<p>Eigenvalue and Eigenvector–based decomposition parameters image: (<b>a</b>) Entropy (H); and (<b>b</b>) angle alpha image.</p>
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<p>Eigenvalue- and Eigenvector-based parameter: (<b>a</b>) Anisotropy (A) and (<b>b</b>) RGB image of H-A-Alpha(α) decomposition modelling.</p>
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<p>Yamaguchi four-component decomposition for DFSAR data: (<b>a</b>) full view of the study area, Erlanger Crater; and (<b>b</b>) closed view of the study area showing three types of scattering, namely, surface, double bounce, and volumetric.</p>
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<p>CPR value of Erlanger Crater: (<b>a</b>) Mini-SAR data—Chandrayaan-1; and (<b>b</b>) DFSAR data—Chandrayaan-2.</p>
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29 pages, 10852 KiB  
Article
Resource-Exploration-Oriented Lunar Rocks Monocular Detection and 3D Pose Estimation
by Jiayu Suo, Hongfeng Long, Yuebo Ma, Yuhao Zhang, Zhen Liang, Chuan Yan and Rujin Zhao
Aerospace 2025, 12(1), 4; https://doi.org/10.3390/aerospace12010004 - 25 Dec 2024
Viewed by 432
Abstract
Lunar in situ resource utilization is a core goal in lunar exploration, with accurate lunar rock pose estimation being essential. To address the challenges posed by the lack of texture features and extreme lighting conditions, this study proposes the Simulation-YOLO-Hourglass-Transformer (SYHT) method. The [...] Read more.
Lunar in situ resource utilization is a core goal in lunar exploration, with accurate lunar rock pose estimation being essential. To address the challenges posed by the lack of texture features and extreme lighting conditions, this study proposes the Simulation-YOLO-Hourglass-Transformer (SYHT) method. The method enhances accuracy and robustness in complex lunar environments, demonstrating strong adaptability and excellent performance, particularly in conditions of extreme lighting and scarce texture. This approach provides valuable insights for object pose estimation in lunar exploration tasks and lays the foundation for lunar resource development. First, the YOLO-Hourglass-Transformer (YHT) network is used to extract keypoint information from each rock and generate the corresponding 3D pose. Then, a lunar surface imaging physics simulation model is employed to generate simulated lunar rock data for testing the method. The experimental results show that the SYHT method performs exceptionally well on simulated lunar rock data, achieving a mean per-joint position error (MPJPE) of 37.93 mm and a percentage of correct keypoints (PCK) of 99.94%, significantly outperforming existing methods. Finally, transfer learning experiments on real-world datasets validate its strong generalization capability, highlighting its effectiveness for lunar rock pose estimation in both simulated and real lunar environments. Full article
(This article belongs to the Section Astronautics & Space Science)
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<p>Comparison between Earth rocks (<b>left</b>) and lunar rocks (<b>right</b>).</p>
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<p>The significant difference between the illumination of the Earth (<b>left</b>) and the illumination of the moon (<b>right</b>).</p>
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<p>Solution to the lack of obvious texture in lunar rocks: results of some methods from the literature [<a href="#B5-aerospace-12-00004" class="html-bibr">5</a>,<a href="#B9-aerospace-12-00004" class="html-bibr">9</a>,<a href="#B10-aerospace-12-00004" class="html-bibr">10</a>,<a href="#B12-aerospace-12-00004" class="html-bibr">12</a>]. Reproduced with permission from Rongxing Li, Kaichang Di, Andrew B. Howard, et al. [<a href="#B7-aerospace-12-00004" class="html-bibr">7</a>], Journal of Field Robotics; published by John Wiley and Sons, 2007.</p>
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<p>Partial results of methods in the literature for addressing extreme lighting conditions in the lunar surface environments [<a href="#B13-aerospace-12-00004" class="html-bibr">13</a>,<a href="#B14-aerospace-12-00004" class="html-bibr">14</a>,<a href="#B17-aerospace-12-00004" class="html-bibr">17</a>].</p>
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<p>SYHT overall process diagram.</p>
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<p>The process of YHT. The left side shows the architecture of the lunar rock keypoint detection model, which utilizes the YOLOv5 backbone network (CSPDarknet), the feature fusion module (Neck-PANet), and the Head–Yolo layer to process the input images and output detection results. The right side illustrates the lunar rock pose estimation process, which includes spatial pooling and clustering steps to generate representative tokens. These tokens are then used with learnable tokens and a cross-attention mechanism to estimate the pose of the lunar rocks.</p>
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<p>Simulation method flowchart.</p>
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<p>Top view of lunar surface.</p>
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<p>Simulated monthly environment display diagram.</p>
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<p>Original image (<b>left</b>): presenting rock and pit features in a grayish white color scheme; depth information map (<b>middle</b>): highlighting the depth changes on the lunar surface through different gray levels, with varying shades of gray representing different heights of terrain (with darker gray representing lower terrain and lighter gray representing higher terrain), and purple being used to emphasize the position of rocks; occlusion map (<b>right</b>): uses orange to represent the background area (non-target area), and purple to highlight the target object (lunar rock).</p>
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<p>BP_LightStudio blueprint.</p>
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<p>Camera event blueprint.</p>
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<p>Comparison of detection results of Yolov5 models.</p>
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<p>Comparison results of YHT module (ours) with other advanced methods.</p>
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<p>Partial display of our simulation data pose estimation results.</p>
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<p>Partial display of publicly available simulation data pose estimation results.</p>
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<p>Partial display of real data pose estimation results.</p>
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11 pages, 540 KiB  
Article
Research on Waveform Adaptability Based on Lunar Channels
by Min Jia, Jonghui Li, Zijie Wang, Chao Zhao, Daifu Yan, Hui Wang, Dongmei Li and Weiran Sun
Electronics 2024, 13(24), 5047; https://doi.org/10.3390/electronics13245047 - 22 Dec 2024
Viewed by 488
Abstract
In recent years, the focus of space research and exploration by various countries and international space agencies has been on the return of humans to the moon. Astronauts on lunar missions need to utilize network communication and exchange data. Against this backdrop, it [...] Read more.
In recent years, the focus of space research and exploration by various countries and international space agencies has been on the return of humans to the moon. Astronauts on lunar missions need to utilize network communication and exchange data. Against this backdrop, it is necessary to consider the performance of communication systems and the extreme conditions of the lunar environment, such as signal attenuation and frequency selection, to ensure the reliability and stability of communication systems. Therefore, providing technical performance adapted to the lunar environment is crucial. In this article, we investigated the applicability of Orthogonal Frequency Division Multiple Access (OFDMA) and Single-Carrier Frequency Division Multiple Access (SC-FDMA) waveforms in the lunar communication environment. Specifically, we used Peak-to-Average Power Ratio (PAPR) and Bit Error Rate (BER) as performance indicators. By studying the impact of different modulation schemes and cyclic prefix lengths on communication performance, we completed the research on waveform adaptability based on lunar channels. Simulation results indicate that the transmission structure we designed can meet the system-level performance requirements of lunar communications. This research provides valuable insights for the design and optimization of communication systems for future lunar missions, paving the way for the seamless integration of advanced ground technologies in extraterrestrial environments. Full article
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<p>Propagation path of lunar electromagnetic waves.</p>
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<p>BER performance versus the length of CP. (<b>a</b>) Uplink BER performance versus the length of CP in 20 MHz bandwidth. (<b>b</b>) Downlink BER performance versus the length of CP in 20 MHz bandwidth. (<b>c</b>) Uplink BER performance versus the length of CP in 10 MHz bandwidth. (<b>d</b>) Downlink BER performance versus the length of CP in 10 MHz bandwidth.</p>
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<p>Performance comparison of different modulation methods. (<b>a</b>) Performance comparison of different modulation methods for 20 M bandwidth. (<b>b</b>) Performance comparison of different modulation methods for 10 M bandwidth.</p>
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<p>Comparison of PAPR for different modulation schemes and orders. (<b>a</b>) Comparison of PAPR for different modulation schemes under 20 MHz bandwidth. (<b>b</b>) Comparison of PAPR for different modulation orders of QAM under 20 MHz bandwidth. (<b>c</b>) Comparison of PAPR for different modulation orders of APSK under 20 MHz bandwidth. (<b>d</b>) Comparison of PAPR for different modulation orders of PSK under 20 MHz bandwidth.</p>
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<p>Comparison of PAPR for different modulation schemes and orders. (<b>a</b>) Comparison of PAPR for different modulation schemes under 10MHz bandwidth. (<b>b</b>) Comparison of PAPR for different modulation orders of QAM under 10MHz bandwidth. (<b>c</b>) Comparison of PAPR for different modulation orders of APSK under 10MHz bandwidth. (<b>d</b>) Comparison of PAPR for different modulation orders of PSK under 10MHz bandwidth.</p>
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<p>Comparison of PAPR for different modulation schemes and orders. (<b>a</b>) Comparison of PAPR for different modulation schemes under 10MHz bandwidth. (<b>b</b>) Comparison of PAPR for different modulation orders of QAM under 10MHz bandwidth. (<b>c</b>) Comparison of PAPR for different modulation orders of APSK under 10MHz bandwidth. (<b>d</b>) Comparison of PAPR for different modulation orders of PSK under 10MHz bandwidth.</p>
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<p>Comparison of BER performance for different modulation schemes. (<b>a</b>) Comparison of QAM and PSK modulation BER performance in 20 MHz bandwidth. (<b>b</b>) Comparison of BER performance for different modulation schemes in 20 MHz bandwidth. (<b>c</b>) Comparison of QAM and PSK modulation BER performance in 10 MHz bandwidth. (<b>d</b>) Comparison of QAM and PSK modulation BER performance in 10 MHz bandwidth.</p>
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<p>Comparison of BER performance for different modulation schemes. (<b>a</b>) Comparison of QAM and PSK modulation BER performance in 20 MHz bandwidth. (<b>b</b>) Comparison of BER performance for different modulation schemes in 20 MHz bandwidth. (<b>c</b>) Comparison of QAM and PSK modulation BER performance in 10 MHz bandwidth. (<b>d</b>) Comparison of QAM and PSK modulation BER performance in 10 MHz bandwidth.</p>
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23 pages, 14898 KiB  
Article
Methods for the Construction and Editing of an Efficient Control Network for the Photogrammetric Processing of Massive Planetary Remote Sensing Images
by Xin Ma, Chun Liu, Xun Geng, Sifen Wang, Tao Li, Jin Wang, Pengying Liu, Jiujiang Zhang, Qiudong Wang, Yuying Wang, Yinhui Wang and Zhen Peng
Remote Sens. 2024, 16(23), 4600; https://doi.org/10.3390/rs16234600 - 7 Dec 2024
Viewed by 489
Abstract
Planetary photogrammetry remains an important technical means of producing high-precision planetary maps. High-quality control networks are fundamental to successful bundle adjustment. However, current software tools used by the planetary mapping community to construct and edit control networks exhibit very low efficiency. Moreover, redundant [...] Read more.
Planetary photogrammetry remains an important technical means of producing high-precision planetary maps. High-quality control networks are fundamental to successful bundle adjustment. However, current software tools used by the planetary mapping community to construct and edit control networks exhibit very low efficiency. Moreover, redundant and invalid control points in the control network can further increase the time required for the bundle adjustment process. Due to a lack of targeted algorithm optimization, existing software tools and methods are unable to meet the photogrammetric processing requirements of massive planetary remote sensing images. To address these issues, we first proposed an efficient control network construction framework based on approximate orthoimage matching and hash quick search. Next, to effectively reduce the redundant control points in the control network and decrease the computation time required for bundle adjustment, we then proposed a control network-thinning algorithm based on a K-D tree fast search. Finally, we developed an automatic detection method based on ray tracing for identifying invalid control points in the control network. To validate the proposed methods, we conducted photogrammetric processing experiments using both the Lunar Reconnaissance Orbiter (LRO) narrow-angle camera (NAC) images and the Origins Spectral Interpretation Resource Identification Security Regolith Explorer (OSIRIS-REx) PolyCam images; we then compared the results with those derived from the famous open-source planetary photogrammetric software, the United States Geological Survey (USGS) Integrated Software for Imagers and Spectrometers (ISIS) version 8.0.0. The experimental results demonstrate that the proposed methods significantly improve the efficiency and quality of constructing control networks for large-scale planetary images. For thousands of planetary images, we were able to speed up the generation and editing of the control network by more than two orders of magnitude. Full article
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<p>The overall process of constructing the control network.</p>
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<p>Schematic diagram of the control network construction process after image matching to obtain control points. Since the three control points shown in the left part of the figure are corresponding points, they need to be merged into a single control point.</p>
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<p>Flowchart of control network construction using the exhaustive search method.</p>
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<p>Hash key generation process (<b>a</b>) and example of a hash table (<b>b</b>). The hash key represents the ID of the control measure. If the hash values of two control measures are the same, they belong to the same control point.</p>
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<p>Flowchart of control network construction based on hash processing.</p>
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<p>Workflow of the K-D tree thinning algorithm (having acquired 3D ground coordinates).</p>
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<p>Diagram of invalid control points. (<b>a</b>) When the image’s EO parameters are inaccurate, control points near the edge of the valid texture region cannot intersect with the celestial body (The line segments represent the calculated light rays). (<b>b</b>) Illustration of two control measures on asteroid Bennu’s surface that cannot intersect the celestial body; the red cross marks indicate the same invalid feature point. The invalid control point fails to compute its ground coordinates due to the low accuracy of the initial EO parameters and the inaccurate shape model of the celestial body (green crosses represent control points).</p>
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<p>Flowchart for removing invalid control points.</p>
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<p>Distribution of images in Dataset 1 over the lunar South Pole (the colored outlines indicate the images, and the base map is the lunar LROC WAC orthoimage provided by NASA [<a href="#B43-remotesensing-16-04600" class="html-bibr">43</a>]).</p>
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<p>Distribution of images in Dataset 2 (the colored outlines represent the test images, and the base map is the Bennu OSIRIS-REx OCAMS global image mosaic provided by the USGS Astrogeology Science Center [<a href="#B44-remotesensing-16-04600" class="html-bibr">44</a>]).</p>
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<p>Distribution of images in Dataset 3, covering the entire surface of the asteroid Bennu (the colored outlines represent the images).</p>
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<p>Time statistics for the construction of a control network using different algorithms. The vertical axis represents the time required to construct the control network. A logarithmic scale is used to enhance the visibility of smaller values due to the significant differences in computation time.</p>
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<p>Time statistics for thinning control networks using different algorithms. Similarly, the vertical axis represents computation time (a logarithmic scale is used to enhance the visibility of smaller values due to significant differences in computation time), and the horizontal axis shows the number of control points processed.</p>
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<p>Distribution of control points on the single image before and after thinning the control network of Dataset 1 (green crosses represent control points the red box highlights the differences between the two methods).</p>
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<p>Distribution of control points on each image before and after thinning of the control network of Dataset 2 (areas without control points are due to a lack of overlap between images or poor image quality; green crosses represent control points; the red box highlights the differences between the two methods).</p>
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<p>Distribution of control points on each image before and after thinning for the control network of Dataset 3 (the colored outlines represent the images).</p>
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<p>Illustration of the identified invalid control points on a single image from Dataset 3, where the green cross marks represent valid control points, and the red cross marks indicate the invalid control points identified by our method.</p>
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<p>Sigma 0 of the bundle adjustment before and after thinning.</p>
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<p>Image mosaic results of adjacent orthoimages (light blue arrows indicate seam lines).</p>
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19 pages, 16179 KiB  
Article
Carbon Nanotube Reinforced Lunar-Based Geopolymer: Curing Conditions
by Janell Prater and Young Hoon Kim
J. Compos. Sci. 2024, 8(12), 492; https://doi.org/10.3390/jcs8120492 - 25 Nov 2024
Viewed by 735
Abstract
Current space exploration focuses on returning to the Moon to expand space exploration capacity by improving technology. The long-term presence of humans and robots on the Moon requires the development of durable habitats for space missions. In recent decades, in situ resource utilization [...] Read more.
Current space exploration focuses on returning to the Moon to expand space exploration capacity by improving technology. The long-term presence of humans and robots on the Moon requires the development of durable habitats for space missions. In recent decades, in situ resource utilization (ISRU) for construction materials has been recognized as a viable option. However, the addition of nanomaterials, which exhibit a high strength-to-weight ratio, has not been incorporated with the ISRU framework in space missions. This paper investigates the impact of carbon nanotubes (CNTs) on lunar simulant-based geopolymers’ compressive strength and water retention. The evaluation of water retention indicates another potential in water recapturing capability. In this study, CNTs can enhance the mechanical properties of lunar simulant-based geopolymer. Two lunar simulants were used, representing the Highland and Mare regions of the Moon. Experimental variables included CNT concentration, four curing regimes (ambient curing, two oven-curing methods, and microwave radiation), and dispersion time in aqueous solutions. Results showed that CNTs can positively influence both strength gain and water retention during curing regimes, but the extent of influence appears to be dependent on simulant type and curing regime. The Highland simulant consistently outperformed the Mare simulant in oven-curing regimes from a strength perspective, regardless of CNT presence. The strength benefits of CNTs were more pronounced at ambient curing temperatures. Even under poor curing conditions—where water availability may be limited at temperatures of 80 °C—CNTs aid in retaining water within the geopolymer matrix, leading to improved strength compared to counterparts. Under the same conditions, a higher concentration of CNTs further confirmed their role in water retention during geopolymerization, with consistently greater water retention observed in samples containing CNTs. Additionally, microwave radiation was explored as an alternative to conventional oven drying, showing potential for reducing curing duration. Finally, the findings suggest that combining CNTs and microwave radiation could enhance water recovery and reuse, contributing to the development of high-strength infrastructure materials on the Moon with reduced energy and cost requirements. Full article
(This article belongs to the Special Issue Novel Cement and Concrete Materials)
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<p>The concepts of geopolymerization and water release; nanomaterial—CNTs.</p>
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<p>Mixture proportion details; (<b>a</b>) mixture proportion of geopolymer with 0%, 0.16%, and 0.32% CNTs (modified from [<a href="#B37-jcs-08-00492" class="html-bibr">37</a>]); (<b>b</b>) prior and current study: water/binder ratio versus compressive strength with varied molarity of NaOH (circle size relative to pH value) in prior literature.</p>
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<p>Test program overview.</p>
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<p>The average compressive strength, in order of strength from lowest to highest.</p>
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<p>CNT effects in each curing regime: (<b>a</b>) A series; (<b>b</b>) H series; (<b>c</b>) W series.</p>
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<p>CSM-M series versus CSM-H series: compressive strength (<math display="inline"><semantics> <mrow> <msubsup> <mrow> <mi>f</mi> </mrow> <mrow> <mi>c</mi> </mrow> <mrow> <mo>′</mo> </mrow> </msubsup> <mo>)</mo> </mrow> </semantics></math>.</p>
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<p>The weight loss and evaporated water (%) in matrices: (<b>a</b>) control; (<b>b</b>) test.</p>
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<p>Weight loss (equivalent to evaporable water) in grams over time (CSM-M series).</p>
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<p>Apparent density versus compressive strength (<math display="inline"><semantics> <mrow> <msubsup> <mrow> <mi>f</mi> </mrow> <mrow> <mi>c</mi> </mrow> <mrow> <mo>′</mo> </mrow> </msubsup> <mo>)</mo> </mrow> </semantics></math>.</p>
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<p>SEM images on the selected samples: (<b>a</b>) CSM-H-0-N; (<b>b</b>) CSM-W-0.16-8; (<b>c</b>) JSC-W-0-N and JSC-W-0.16-8; (<b>d</b>) CSM-M-0.32-8.</p>
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<p>SEM images on the selected samples: (<b>a</b>) CSM-H-0-N; (<b>b</b>) CSM-W-0.16-8; (<b>c</b>) JSC-W-0-N and JSC-W-0.16-8; (<b>d</b>) CSM-M-0.32-8.</p>
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