Nonlinear receding horizon guidance for spacecraft formation reconfiguration on libration point orbits using a symplectic numerical method
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- 作者：Haijun Peng ; hjpeng@dlut.edu.cn" class="auth_mail" title="E-mail the corresponding author ; Xin Jiang
- 关键词：Spacecraft formation reconfiguration ; Libration point orbits ; Circular restricted three body problem ; Guidance strategy ; Nonlinear receding horizon control ; Symplectic numerical method
- 刊名：ISA Transactions
- 出版年：2016
- 出版时间：January 2016
- 年：2016
- 卷：60
- 期：Complete
- 页码：38-52
- 全文大小：4089 K
文摘
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SFR on libration orbits are implemented successfully by nonlinear RHC guidance.
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A symplectic iteration algorithm is proposed for rapidly solving nonlinear RHC.
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Symplectic iteration algorithm reduces the parameter sensitivities of nonlinear RHC.
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Nonlinear RHC compared with LQTC has obvious advantage on convergence and accuracy.