Lu et al., 2021 - Google Patents
Vehicle-borne non-strapdown transfer alignment method and application with poor attitude observation informationLu et al., 2021
- Document ID
- 2325220384738183542
- Author
- Lu J
- Ye L
- Luo W
- Dong J
- Han S
- Publication year
- Publication venue
- Measurement
External Links
Snippet
For transfer alignment in elevation maneuver, the system accuracy will be decreased or divergent because of the poor attitude observation information. What is the impact on the transfer alignment with poor attitude observation information caused by non-strapdown …
- 238000004088 simulation 0 abstract description 39
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
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/53—Determining attitude
-
- 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
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
-
- 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
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/26—Navigation; Navigational instruments not provided for in preceding groups specially adapted for navigation in a road network
- G01C21/28—Navigation; Navigational instruments not provided for in preceding groups specially adapted for navigation in a road network with correlation of data from several navigational instruments
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Xiaojuan et al. | A SINS/CNS deep integrated navigation method based on mathematical horizon reference | |
Liu et al. | An initial alignment method for strapdown gyrocompass based on gravitational apparent motion in inertial frame | |
Li et al. | A calibration method of DVL in integrated navigation system based on particle swarm optimization | |
CN106840151B (en) | Model-free deformation of hull measurement method based on delay compensation | |
Liu et al. | A fast and high-accuracy transfer alignment method between M/S INS for ship based on iterative calculation | |
CN105737823A (en) | GPS/SINS/CNS integrated navigation method based on five-order CKF | |
Lu et al. | Analytic coarse transfer alignment based on inertial measurement vector matching and real-time precision evaluation | |
Zhang et al. | Ship navigation via GPS/IMU/LOG integration using adaptive fission particle filter | |
Gong et al. | An innovational transfer alignment method based on parameter identification UKF for airborne distributed POS | |
Gong et al. | Maneuver-free approach to range-only initial relative orbit determination for spacecraft proximity operations | |
Zhao et al. | A robust filtering algorithm for integrated navigation system of aerospace vehicle in launch inertial coordinate | |
Ning et al. | Initial position and attitude determination of lunar rovers by INS/CNS integration | |
Chen et al. | New rapid transfer alignment method for SINS of airborne weapon systems | |
Wang et al. | Improved whale optimization-based parameter identification algorithm for dynamic deformation of large ships | |
Lu et al. | Vehicle-borne non-strapdown transfer alignment method and application with poor attitude observation information | |
Li et al. | Fast fine initial self-alignment of INS in erecting process on stationary base | |
Zhang et al. | On-orbit real-time magnetometer bias determination for micro-satellites without attitude information | |
Lu et al. | A dynamic precision evaluation method for the star sensor in the stellar-inertial navigation system | |
Yang et al. | A SINS/CNS integrated navigation scheme with improved mathematical horizon reference | |
Liang et al. | An quantitative method for observability analysis and its application in SINS calibration | |
Xu et al. | A SE (2)-based transfer alignment for large installation misalignment angle | |
Lu et al. | In-motion initial alignment and positioning with INS/CNS/ODO integrated navigation system for lunar rovers | |
He et al. | A model-free hull deformation measurement method based on attitude quaternion matching | |
Sheng et al. | A marine SINS transfer alignment method based on group affine of nonlinear state error in local-level frame | |
Ben et al. | System reset of strapdown INS for pipeline inspection gauge |