H∞ control option for a combined energy and attitude control system

作者: Ying Siang Ban , Renuganth Varatharajoo

DOI: 10.1016/J.ASR.2013.07.006

关键词: Attitude controlControl theorySpace researchOptimal controlComputer scienceControl (management)Work (physics)FlywheelEnergy (signal processing)Hybrid system

摘要: A combined energy and attitude control system (CEACS) is a hybrid that uses flywheels to store provide simultaneous in satellites. Previous work appeared Advances Space Research (ASR) employing the proportional-derivative (PD) has proven CEACS works well achieves its mission requirement. However, in-orbit performance uncertainties present challenge pointing capability. Thus, this paper complements previous mentioned work, focuses on H∞ optimal solution for enhancement. The mathematical model numerical treatments architecture are presented. Numerical results show better accuracy at least up 0.043° can be achieved with method.

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