Feedback control of a spacecraft electro-dynamic thruster
نویسندگان
چکیده
منابع مشابه
Adaptive Control of a Spin-Stabilized Spacecraft Using two Reaction Wheels and a 1DoF Gimbaled-Thruster
In impulsive orbital maneuvers, a large disturbance torque is generated by the thrust vector misalignment from the center of mass (C.M). The purpose of this paper is to reject the mentioned disturbance and stabilize the spacecraft attitude, based on the combination of a one degree of freedom (1DoF) gimbaled-thruster, two reaction wheels (RWs) and spin-stabilization. In this paper, the disturban...
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ژورنال
عنوان ژورنال: Acta Astronautica
سال: 2020
ISSN: 0094-5765
DOI: 10.1016/j.actaastro.2020.03.043