Nonlinear feedforward control for spacecraft relative attitude tracking

Yujia Tie; Wei Yang; Xiaokui Yue

doi:10.3780/j.issn.1000-758X.2011.06.003

Nonlinear feedforward control for spacecraft relative attitude tracking

Yujia Tie, Wei Yang, Xiaokui Yue

School of Astronautics

Northwestern Polytechnical University Xian

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

Abstract

The spacecraft relative attitude kinematics and dynamics based on modified rodrigues parameters (MRP) were proposed in the presence of serious nonlinear and controller design complexity during spacecraft relative attitude tracking control. A nonlinear feedforward controller was designed using Lyapunov method. The control law can not only ensure global asymptotic steady of close-loop system, but also make relative attitude tracking errors converge to zero field speedily. By using Matlab/Simulink programming, the modeling and simulation of spacecraft relative attitude tracking were discussed. Numerical simulations are exploited to verify the effectiveness of the model and control law.

Original language	English
Pages (from-to)	15-20
Number of pages	6
Journal	Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology
Volume	31
Issue number	6
DOIs	https://doi.org/10.3780/j.issn.1000-758X.2011.06.003
State	Published - Dec 2011

Keywords

Attitude tracking
Lagrange equation
Modified rodrigues parameters
Nonlinear control
Spacecraft

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10.3780/j.issn.1000-758X.2011.06.003

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title = "Nonlinear feedforward control for spacecraft relative attitude tracking",

abstract = "The spacecraft relative attitude kinematics and dynamics based on modified rodrigues parameters (MRP) were proposed in the presence of serious nonlinear and controller design complexity during spacecraft relative attitude tracking control. A nonlinear feedforward controller was designed using Lyapunov method. The control law can not only ensure global asymptotic steady of close-loop system, but also make relative attitude tracking errors converge to zero field speedily. By using Matlab/Simulink programming, the modeling and simulation of spacecraft relative attitude tracking were discussed. Numerical simulations are exploited to verify the effectiveness of the model and control law.",

keywords = "Attitude tracking, Lagrange equation, Modified rodrigues parameters, Nonlinear control, Spacecraft",

author = "Yujia Tie and Wei Yang and Xiaokui Yue",

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AU - Yang, Wei

AU - Yue, Xiaokui

PY - 2011/12

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N2 - The spacecraft relative attitude kinematics and dynamics based on modified rodrigues parameters (MRP) were proposed in the presence of serious nonlinear and controller design complexity during spacecraft relative attitude tracking control. A nonlinear feedforward controller was designed using Lyapunov method. The control law can not only ensure global asymptotic steady of close-loop system, but also make relative attitude tracking errors converge to zero field speedily. By using Matlab/Simulink programming, the modeling and simulation of spacecraft relative attitude tracking were discussed. Numerical simulations are exploited to verify the effectiveness of the model and control law.

AB - The spacecraft relative attitude kinematics and dynamics based on modified rodrigues parameters (MRP) were proposed in the presence of serious nonlinear and controller design complexity during spacecraft relative attitude tracking control. A nonlinear feedforward controller was designed using Lyapunov method. The control law can not only ensure global asymptotic steady of close-loop system, but also make relative attitude tracking errors converge to zero field speedily. By using Matlab/Simulink programming, the modeling and simulation of spacecraft relative attitude tracking were discussed. Numerical simulations are exploited to verify the effectiveness of the model and control law.

KW - Attitude tracking

KW - Lagrange equation

KW - Modified rodrigues parameters

KW - Nonlinear control

KW - Spacecraft

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JF - Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology

IS - 6

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Nonlinear feedforward control for spacecraft relative attitude tracking

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