Optimal Guidance for Lunar Module Soft Landing
In this paper, we consider an optimal control problem arising from the optimal guidance of a lunar module to achieving soft landing, where the description of the system dynamics is in a three-dimensional coordinate system. Our aim is to construct an optimal guidance law to realize the soft landing o...
| Main Authors: | , , , |
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| Format: | Journal Article |
| Published: |
InforMath publishing group
2010
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| Subjects: | |
| Online Access: | http://hdl.handle.net/20.500.11937/9905 |