A predictive control algorithm for spacecraft attitude maneuver with nonconvex geometric constraint

Xiao Jun Cheng; Hu Tao Cui; Ping Yuan Cui; Rui Xu

doi:10.3873/j.issn.1000-1328.2011.05.016

A predictive control algorithm for spacecraft attitude maneuver with nonconvex geometric constraint

Xiao Jun Cheng^*, Hu Tao Cui, Ping Yuan Cui, Rui Xu

^*Corresponding author for this work

School of Aerospace Engineering

Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

16 Citations (Scopus)

Abstract

A predictive control algorithm is presented in this paper for spacecraft attitude maneuver with nonconvex geometric constraint and bounded inputs. The nonconvex property of the geometric constraint is proved based on the analysis of its Hessian matrix. Then the transformation from nonconvex constraint to convex one is presented by constructing positive definite Hessian matrix. Consequently, a predictive control algorithm for spacecraft attitude maneuver is presented, and it can readily obtain global solution, as well as to solve the safety problem. The simulation results show that the presented algorithm can achieve optimal attitude path and satisfy all constraints.

Original language	English
Pages (from-to)	1070-1076
Number of pages	7
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	32
Issue number	5
DOIs	https://doi.org/10.3873/j.issn.1000-1328.2011.05.016
Publication status	Published - May 2011

Keywords

Convex planning
Nonconvex constraint
Predictive control
Spacecraft attitude maneuver

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10.3873/j.issn.1000-1328.2011.05.016

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abstract = "A predictive control algorithm is presented in this paper for spacecraft attitude maneuver with nonconvex geometric constraint and bounded inputs. The nonconvex property of the geometric constraint is proved based on the analysis of its Hessian matrix. Then the transformation from nonconvex constraint to convex one is presented by constructing positive definite Hessian matrix. Consequently, a predictive control algorithm for spacecraft attitude maneuver is presented, and it can readily obtain global solution, as well as to solve the safety problem. The simulation results show that the presented algorithm can achieve optimal attitude path and satisfy all constraints.",

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AU - Cheng, Xiao Jun

AU - Cui, Hu Tao

AU - Cui, Ping Yuan

AU - Xu, Rui

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Y1 - 2011/5

N2 - A predictive control algorithm is presented in this paper for spacecraft attitude maneuver with nonconvex geometric constraint and bounded inputs. The nonconvex property of the geometric constraint is proved based on the analysis of its Hessian matrix. Then the transformation from nonconvex constraint to convex one is presented by constructing positive definite Hessian matrix. Consequently, a predictive control algorithm for spacecraft attitude maneuver is presented, and it can readily obtain global solution, as well as to solve the safety problem. The simulation results show that the presented algorithm can achieve optimal attitude path and satisfy all constraints.

AB - A predictive control algorithm is presented in this paper for spacecraft attitude maneuver with nonconvex geometric constraint and bounded inputs. The nonconvex property of the geometric constraint is proved based on the analysis of its Hessian matrix. Then the transformation from nonconvex constraint to convex one is presented by constructing positive definite Hessian matrix. Consequently, a predictive control algorithm for spacecraft attitude maneuver is presented, and it can readily obtain global solution, as well as to solve the safety problem. The simulation results show that the presented algorithm can achieve optimal attitude path and satisfy all constraints.

KW - Convex planning

KW - Nonconvex constraint

KW - Predictive control

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A predictive control algorithm for spacecraft attitude maneuver with nonconvex geometric constraint

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Keywords

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