Iterguidscheitsappllunaland.pdf

spc_stnv_000348

"An Iterative Guidance Scheme and Its Application to Lunar Landing."

TN D-2869

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 under more realistic and accurate assumptions and are not included.

1965-07-01

Saturn V Collection

Box 14, Folder 22

University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama

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spc_stnv_000325_000349

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