Attitude determination and control suitable for micro-spacecraft
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx5/7042/19014/00879284.pdf?arnumber=879284
Cited by 6 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. Development of Control Algorithm and Fabrication of Attitude Determination and Control System for NanoSatellites;2024 1st International Conference on Innovative Sustainable Technologies for Energy, Mechatronics, and Smart Systems (ISTEMS);2024-04-26
2. Open-loop and closed-loop attitude dynamics and controls of miniature spacecraft using pseudowheels;Computers & Mathematics with Applications;2012-09
3. Attitude control of miniature spacecraft under the gravitational effect using a hub-bimorph mechanism;Journal of Vibration and Control;2012-06-27
4. Geometrical Attitude Determination Algorithm Based on Vector Measurements;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2010
5. Mission results for Sapphire, a student-built satellite;Acta Astronautica;2008-04
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