Nonlinear optimal feedback control for lunar module soft landing
In this paper, the task of achieving the soft landing of a lunar module such that the fuel consumption and the flight time are minimized is formulated as an optimal control problem. The motion of the lunar module is described in a three dimensional coordinate system. We obtain the form of the optima...
| Main Authors: | , , , |
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| Format: | Journal Article |
| Published: |
Springer US
2012
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| Online Access: | http://hdl.handle.net/20.500.11937/21189 |