H2 optimal control solution for a combined energy and attitude control system |
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| Institution: | 1. School of Aerospace, Beijing Institute of Technology, No. 5 Zhongguancun South Street, Haidian, Beijing 100081, China\n;2. Department of Mechanical Science and Engineering Graduate School of Engineering, Hiroshima University, 1-4-1 Kagamiyama, Higashihiroshima 739-8527, Japan\n |
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| Abstract: | This addendum is an extension of a series of research work on the combined energy and attitude control system (CEACS) for small satellites. Previous works appeared in Acta Astronautica showed that the CEACS is able to simultaneously perform the attitude control and energy storage task. This addendum focuses on the CEACS attitude control enhancement by employing the H2 optimal control method. Governing equations describing the CEACS H2 attitude control architecture are established. Numerical treatments are performed in order to validate the attitude control option. |
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