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 Astronautics

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

17 Scopus citations

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
State	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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title = "A predictive control algorithm for spacecraft attitude maneuver with nonconvex geometric constraint",

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.",

keywords = "Convex planning, Nonconvex constraint, Predictive control, Spacecraft attitude maneuver",

author = "Cheng, \{Xiao Jun\} and Cui, \{Hu Tao\} and Cui, \{Ping Yuan\} and Rui Xu",

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AU - Cheng, Xiao Jun

AU - Cui, Hu Tao

AU - Cui, Ping Yuan

AU - Xu, Rui

PY - 2011/5

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

KW - Spacecraft attitude maneuver

UR - https://www.scopus.com/pages/publications/79959790993

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JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 5

ER -

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

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Keywords

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