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Finite Time Coordinated Attitude Control for Spacecraft Formation Flying Under Input Saturation
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In this paper, finitetime attitude coordinated control for spacecraft formation flying (SFF) subjected to input saturation is investigated. More specifically, a bounded finitetime state feedback control law is first developed ...
Output Feedback Attitude Tracking for Spacecraft Under Control Saturation and Disturbance
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper proposes a class of velocityfree attitude stable controller using a novel finitetime observer for spacecraft attitude tracking, which explicitly takes into account control input saturation to assure fast and ...