Abstract
This paper documents the development and testing of a fault tolerant sliding mode attitude control algorithm for a nanosatellite with reaction wheel control actuation.
Original language | English |
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DOIs | |
Publication status | Published - 13 Aug 2012 |
Bibliographical note
AIAA Guidance, Navigation, and Control Conference ; Conference date: 13-08-2012 Through 16-08-2012Keywords
- nanosatellite, air bearing tests, fault-tolerant, sliding mode attitude control, unscented Kalman filter