[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Haotian et al., 2020 - Google Patents

Accurate attitude estimation of HB2 standard model based on QNCF in hypersonic wind tunnel test

Haotian et al., 2020

View HTML
Document ID
16474804217594276322
Author
Haotian Y
Bin Z
Qi W
Xiong W
Xiaobin X
Zhang R
Publication year
Publication venue
Chinese Journal of Aeronautics

External Links

Snippet

The accuracy of the HB2 standard model attitude measurement has an important impact on the hypersonic wind tunnel data assessment. The limited size of the model and the existence of external vibrations make it challenging to obtain real-time reliable attitude …
Continue reading at www.sciencedirect.com (HTML) (other versions)

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
    • G01C21/10—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
    • G01C21/20—Instruments for performing navigational calculations
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments and devices referred to in the preceding groups
    • G01C25/005—Manufacturing, calibrating, cleaning, or repairing instruments and devices referred to in the preceding groups initial alignment, calibration or starting-up of inertial devices
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects

Similar Documents

Publication Publication Date Title
Wu et al. Fast complementary filter for attitude estimation using low-cost MARG sensors
Hong Fuzzy logic based closed-loop strapdown attitude system for unmanned aerial vehicle (UAV)
JP5061264B1 (en) Small attitude sensor
CN107560613B (en) Robot indoor track tracking system and method based on nine-axis inertial sensor
Zou et al. A compound control method based on the adaptive neural network and sliding mode control for inertial stable platform
Wu et al. A novel approach for attitude estimation based on MEMS inertial sensors using nonlinear complementary filters
Wang et al. High-order nonlinear differentiator and application to aircraft control
CN105929836B (en) Control method for quadrotor
CN101413800A (en) Navigating and steady aiming method of navigation / steady aiming integrated system
CN106840151B (en) Model-free deformation of hull measurement method based on delay compensation
CN114543794A (en) Absolute positioning method for fusion of visual inertial odometer and discontinuous RTK
Haotian et al. Accurate attitude estimation of HB2 standard model based on QNCF in hypersonic wind tunnel test
CN104121930A (en) Compensation method for MEMS (Micro-electromechanical Systems) gyroscopic drifting errors based on accelerometer coupling
Pan et al. Attitude estimation of miniature unmanned helicopter using unscented kalman filter
Lu et al. Vehicle-borne non-strapdown transfer alignment method and application with poor attitude observation information
Wang et al. Attitude estimation for UAV with low-cost IMU/ADS based on adaptive-gain complementary filter
Tran et al. Dynamical analysis and validation of motion control by filtering performance for aerial robotic system
Wu et al. A novel approach for attitude estimation using MEMS inertial sensors
Qi et al. A state estimator of UAV using time-delayed position and IMU data
Safaeifar et al. Drift cancellation of an orientation tracker for a virtual reality head-mounted display
Qi et al. Imu attitude calculation method based on gradient descent algorithm
Zhang et al. An improved Kalman filter for attitude determination of multi-rotor UAVs based on low-cost MEMS sensors
Che et al. A multi-sensor fusion algorithm for UAV attitude estimation
Ye et al. GNSS-INS-dynamic fusion with robustness to outliers based on external force state estimation
Xiong et al. Installation error calibration for MEMS angular measurement system in hypersonic wind tunnel