In this chapter, we illustrate the applicability of ET-ADRC in attitude tracking for spacecraft systems. Since the kinematic and dynamic equations of rigid spacecraft possess highly coupled nonlinear characteristics and attitude dynamics may suffer from external disturbances, inertia-matrix uncertainties, and even actuator failures, control systems play an important role in achieving attitude maneuvering, attitude tracking, and high-precision pointing of spacecraft, and the attitude-control problem has attracted significant attention over the past few decades [1–5].
Event-Triggered Attitude Tracking for Rigid Spacecraft
Studies in Systems, Decision and Control
16.03.2021
22 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Event-triggered adaptive control for attitude tracking of spacecraft
British Library Online Contents | 2019
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