Coupled orbit-attitude dynamics and trajectory tracking control for spacecraft electromagnetic docking

Volume: 101, Pages: 553 - 572
Published: Jan 1, 2022
Abstract
In this paper, the simplified electromagnetic force/torque model and coupled orbit-attitude dynamics modeling in spacecraft electromagnetic docking are investigated, and an improved sliding mode control scheme based on planned trajectory is proposed. In this scenario, the docking two spacecraft are equipped with four energized solenoids with iron cores fixed in the body frame, and small-angle hypothesis is used to derive the simplified...
Paper Details
Title
Coupled orbit-attitude dynamics and trajectory tracking control for spacecraft electromagnetic docking
Published Date
Jan 1, 2022
Volume
101
Pages
553 - 572
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