SINS/CNS integration algorithm and simulations for extended time flights using linearized Kalman filtering
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/7284653/7296115/07296122.pdf?arnumber=7296122
Cited by 14 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Integrated generation software for dynamic navigation parameters of inertial/star-sensor integrated system;Third International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2023);2023-07-18
2. A High-Precision Indoor Positioning Algorithm via Integration of Pedestrian Dead Reckoning and Visible Light Positioning on Mobile Devices;2023 8th International Conference on Computer and Communication Systems (ICCCS);2023-04-21
3. Research on joint calibration and compensation of the inclinometer installation and instrument errors in the celestial positioning system;Journal of Field Robotics;2022-06-20
4. Accelerometer Bias and Star Sensor Installation Error Joint Calibration for the SINS/CNS Integrated Navigation System Using Attitude Maneuver;Guidance, Navigation and Control;2022-05-05
5. INS’s Error Compensation via Measurement Differencing Kalman Filter;IEEE Transactions on Instrumentation and Measurement;2022
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