Adaptive Controller For Simultaneous Spacecraft Attitude Tracking And Reaction Wheel Fault Detection
arXiv:2504.12124 · doi:10.2514/1.A36424
Abstract
The attitude control of a spacecraft is integral to achieving mission success. However, failures in actuators such as reaction wheels are detrimental and can often lead to an early end of mission. We propose a Lyapunov-based adaptive controller that can estimate and compensate for reaction wheels degradation simultaneously. The controller incorporates an adaptive update control law with a gradient-based term and an integral concurrent learning term that collects input-output data for online estimation of uncertain parameters. The proposed controller guarantees attitude tracking and its performance is tested through numerical simulations.
17 pages, 10 figures