Path shaping guidance for terminal lunar descent

被引:19
|
作者
McInnes, CR
机构
[1] Department of Aerospace Engineering, University of Glasgow, Glasgow
关键词
D O I
10.1016/0094-5765(95)00119-0
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Lunar descent guidance methods are investigated which provide soft landing in regions of undulating terrain. Path shaping guidance is developed to provide a family of descent paths which converge to a soft-landing, but avoid obstructions created by neighbouring terrain. A phase of terrain slope nulling is also considered to aid in the selection of a suitable landing location. These methods may be patched to a conventional gravity turn trajectory for the main braking phase of the descent. Since the guidance commands are provided in closed, analytic form the demands on the on-board flight computer are limited, freeing its capacity for more computationally intensive tasks. In principle, the methods also increase on-board autonomy, allowing more flexible mission operations.
引用
收藏
页码:367 / 377
页数:11
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