2018
DOI: 10.1177/0954410018787417
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Spacecraft formation flying control under orbital perturbations by state-dependent Riccati equation method in the presence of on–off actuators

Abstract: In this paper, spacecraft formation flying control under orbital perturbations by state-dependent Riccati equation method in the presence of on–off actuators is studied. Here, state-dependent Riccati equation is proposed as a more systematic and simple controller for solving the nonlinear problem of spacecraft formation flying in the leader–follower architecture. To create real conditions, the full nonlinear model of motion is considered while orbital perturbations are contained in the model. Also, to consider… Show more

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Cited by 7 publications
(3 citation statements)
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“…[8][9][10] Therefore, the formation reconfiguration control problem has aroused widespread concern recently. [11][12][13] Thrust failure is one of the challenges that must be addressed in spacecraft formation reconfiguration because the controllers designed based on fully actuated dynamics are unsuitable for underactuated cases. 14,15 Various control schemes have been proposed for the underactuated attitude or relative orbital control problem by different approaches.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…[8][9][10] Therefore, the formation reconfiguration control problem has aroused widespread concern recently. [11][12][13] Thrust failure is one of the challenges that must be addressed in spacecraft formation reconfiguration because the controllers designed based on fully actuated dynamics are unsuitable for underactuated cases. 14,15 Various control schemes have been proposed for the underactuated attitude or relative orbital control problem by different approaches.…”
Section: Introductionmentioning
confidence: 99%
“…810 Therefore, the formation reconfiguration control problem has aroused widespread concern recently. 1113…”
Section: Introductionmentioning
confidence: 99%
“…Due to the aforementioned privileges of the SDRE approach on the one hand and the challenges of the coordination control of flexible satellites in a formation on the other hand, it is worthy to study the important problem of flexible spacecraft formation flying coordination control using SDRE technique. The satellites in a formation may be subject to input constraints such as input saturation or on-off input (Fu et al, 2018; Huang and Jia, 2018; Rouzegar et al, 2019).…”
Section: Introductionmentioning
confidence: 99%