Attitude Estimation for Satellite Fault Tolerant System Using Federated Unscented Kalman Filter-Reference-Cited by-同舟云学术

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Attitude Estimation for Satellite Fault Tolerant System Using Federated Unscented Kalman Filter

Published:2010-06-15 Issue:2 Volume:11 Page:80-86
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:International Journal of Aeronautical and Space Sciences

Author:

Bae Jong-Hee,Kim You-Dan

Publisher

The Korean Society for Aeronautical & Space Sciences

Link

http://ocean.kisti.re.kr/downfile/crosscheck/ksass/JAKO201021751975403.pdf

Cited by 27 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. Distributed fusion fault-tolerant attitude estimation scheme for nanosatellite using commercial off-the-shelf sensors;Advances in Space Research;2022-12

2. Sensor fault-tolerant attitude determination system based on the nonlinear interacting-multiple-model approach;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-08-17

3. An attitude estimation scheme for nanosatellite using micro sensors based on decentralized information fusion;Optik;2021-08

4. Verification of nonlinear state observer system for RazakSAT using extended Kalman filter;PROCEEDINGS OF 8TH INTERNATIONAL CONFERENCE ON ADVANCED MATERIALS ENGINEERING & TECHNOLOGY (ICAMET 2020);2021

5. A Fault-Tolerant Data Fusion Method of MEMS Redundant Gyro System Based on Weighted Distributed Kalman Filtering;Micromachines;2019-04-26

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