Adaptive nonlinear robust relative pose control of spacecraft autonomous rendezvous and proximity operations
被引:15
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作者:
Sun, Liang
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Beihang Univ, Sch Automat Sci & Elect Engn, Res Div Sci & Technol 7, Aircraft Control Lab, Beijing 100191, Peoples R China
Beihang Univ, Res Div 7, Xueyuan Rd 37, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Automat Sci & Elect Engn, Res Div Sci & Technol 7, Aircraft Control Lab, Beijing 100191, Peoples R China
Sun, Liang
[1
,3
]
Huo, Wei
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h-index: 0
机构:
Beihang Univ, Sch Automat Sci & Elect Engn, Res Div Sci & Technol 7, Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Automat Sci & Elect Engn, Res Div Sci & Technol 7, Aircraft Control Lab, Beijing 100191, Peoples R China
Huo, Wei
[1
]
Jiao, Zongxia
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h-index: 0
机构:
Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Automat Sci & Elect Engn, Res Div Sci & Technol 7, Aircraft Control Lab, Beijing 100191, Peoples R China
Jiao, Zongxia
[2
]
机构:
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Res Div Sci & Technol 7, Aircraft Control Lab, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
[3] Beihang Univ, Res Div 7, Xueyuan Rd 37, Beijing 100191, Peoples R China
This paper studies relative pose control for a rigid spacecraft with parametric uncertainties approaching to an unknown tumbling target in disturbed space environment. State feedback controllers for relative translation and relative rotation are designed in an adaptive nonlinear robust control framework. The element-wise and norm-wise adaptive laws are utilized to compensate the parametric uncertainties of chaser and target spacecraft, respectively. External disturbances acting on two spacecraft are treated as a lumped and bounded perturbation input for system. To achieve the prescribed disturbance attenuation performance index, feedback gains of controllers are designed by solving linear matrix inequality problems so that lumped disturbance attenuation with respect to the controlled output is ensured in the L(2-)gain sense. Moreover, in the absence of lumped disturbance input, asymptotical convergence of relative pose are proved by using the Lyapunov method. Numerical simulations are performed to show that position tracking and attitude synchronization are accomplished in spite of the presence of couplings and uncertainties. (C) 2016 ISA. Published by Elsevier Ltd. All rights reserved.
机构:
Beihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
Sun, Liang
Huo, Wei
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
Huo, Wei
Jiao, Zongxia
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
机构:
Beihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R ChinaBeihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
Sun, Liang
Zheng, Zewei
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R ChinaBeihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
机构:
Beihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
Sun, Liang
Zheng, Zewei
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
机构:
Beihang Univ, Sci & Technol Aircraft Control Lab, Div Res 7, Beijing 100191, Peoples R ChinaBeihang Univ, Sci & Technol Aircraft Control Lab, Div Res 7, Beijing 100191, Peoples R China
Sun, Liang
Huo, Wei
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Sci & Technol Aircraft Control Lab, Div Res 7, Beijing 100191, Peoples R ChinaBeihang Univ, Sci & Technol Aircraft Control Lab, Div Res 7, Beijing 100191, Peoples R China
机构:
Beihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
Sun, Liang
Huo, Wei
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R ChinaBeihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
机构:
Beihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R ChinaBeihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
Sun, Liang
Huo, Wei
论文数: 0引用数: 0
h-index: 0
机构:
Beihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R ChinaBeihang Univ, Res Div 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China