Anti‐unwinding adaptive spacecraft attitude tracking control based on similar skew‐symmetric structures

This article addresses the adaptive attitude tracking control based on similar skew‐symmetric structure. Based on the structure, a novel adaptive backstepping scheme is proposed to design the attitude controller. To avoid unwinding, a rotation matrix rather than a quaternion is used to describe the...

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Veröffentlicht in:	International journal of robust and nonlinear control 2022-05, Vol.32 (7), p.4438-4458
Hauptverfasser:	Su, Yunzhe, Yang, Yajun, Yang, Xuerong, Zhang, Xueyang
Format:	Artikel
Sprache:	eng
Schlagworte:	Adaptive control anti‐unwinding backstepping Control systems design Euclidean geometry Euclidean space input‐to‐state stable Liapunov functions Quaternions similar skew‐symmetric structure smooth projection function Spacecraft attitude control spacecraft attitude tracking Spacecraft tracking Tracking control
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