An adaptive control for hybrid thrusters and reaction wheels strategy

The quaternion-based, high precision, large angle rapid reorientation of rigid spacecraft is the main problem investigated in this study. The operation is accomplished via a hybrid thrusters and reaction wheels strategy where thrusters are engaged in providing a primary maneuver torque in open loop, while reaction wheels provide fine control torque to achieve high precision in closed-loop control. The inaccuracy of thrusters is handled by an adaptive control. Detailed proofs and numerical simulation examples are presented to illustrate all the technical aspects of this work.