Fixed-Time Attitude Tracking Control for Rigid Spacecraft With Actuator Misalignments and Faults

This paper investigates an attitude tracking maneuver problem for a rigid spacecraft with external disturbances, uncertain inertia parameters, actuator misalignments, and faults. First, all the uncertainty terms are split from the desired commanded control torque, and then, the nonsingular terminal...

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Bibliographic Details
Main Authors: Jiwei Gao, Sen Zhang, Zhumu Fu
Format: Article
Published: IEEE 2019-01-01
Series:IEEE Access
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