2020
DOI: 10.1007/s11432-020-2916-8
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Observer-based multi-objective parametric design for spacecraft with super flexible netted antennas

Abstract: A multi-objective parametric design method that based on the robust observer is proposed for the attitude control of satellites with super flexible netted antennas. First, a parametric observer-based controller is obtained based on the eigen-structure assignment theory. The closed-loop poles are assigned to desired positions or regions, and full degrees of freedom of the design, which are characterized by a set of parameters, are preserved under the proposed control law. Second, the obtained parameters are com… Show more

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Cited by 14 publications
(20 citation statements)
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References 28 publications
(123 reference statements)
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“…These degrees of freedom can be properly utilised to achieve additional system performance (see, e.g. Duan, 1992Duan, , 1993Duan et al, 2000, 2002, and Duan & Zhao, 2020.…”
Section: Decoupled Designmentioning
confidence: 99%
“…These degrees of freedom can be properly utilised to achieve additional system performance (see, e.g. Duan, 1992Duan, , 1993Duan et al, 2000, 2002, and Duan & Zhao, 2020.…”
Section: Decoupled Designmentioning
confidence: 99%
“…All these degrees of freedom can be further utilised to achieve the additional performance of the system (see, e.g. Duan, 1992Duan, , 1993Duan & Zhao, 2020;Duan et al, 2000Duan et al, , 2002.…”
Section: Solutions Ofmentioning
confidence: 99%
“…All these degrees of freedom can be further utilised to achieve additional performance of the system (see, e.g. Duan, 1992Duan, , 1993Duan et al, 2002Duan et al, , 2000Duan & Zhao, 2020. To end this section, we give the following summingup points:…”
Section: The Closed-loop Systemmentioning
confidence: 99%