Dual-Loop Tube-Based Robust Model Predictive Attitude Tracking Control for Spacecraft With System Constraints and Additive Disturbances

In this article, the problem of optimal time-varying attitude tracking control for rigid spacecraft with system constraints and unknown additive disturbances is considered. Through the design of a new nonlinear tube-based robust model predictive control (TRMPC) algorithm, a dual-loop cascaded tracki...

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Veröffentlicht in:	IEEE transactions on industrial electronics (1982) Jg. 69; H. 4; S. 4022 - 4033
Hauptverfasser:	Chai, Runqi, Tsourdos, Antonios, Gao, Huijun, Xia, Yuanqing, Chai, Senchun
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.04.2022 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Additives Algorithms Attitude control Comparative studies Constraint tightening Control stability Control systems Disturbances Nonlinear feedback Optimal control optimal time-varying attitude tracking Optimization Predictive control Robust control Space vehicles spacecraft Spacecraft attitude control Spacecraft tracking Stability analysis Tracking control Trajectory tube-based robust model predictive control (TRMPC) Vehicle dynamics
ISSN:	0278-0046, 1557-9948
Online-Zugang:	Volltext
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