"An Iterative Guidance Scheme and Its Application to Lunar Landing."
A guidance scheme for vehicle flight from lunar orbit to a prescribed point on a spherical, non-rotating moon is presented. The equations of motion have been simplified only to perm it a closed solution for the thrust magnitude and thrust direction. The trajectory computations them selves are made u...
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| Format: | Electronic |
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University of Alabama in Huntsville Archives
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| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10969 |