"An Iterative Guidance Scheme and Its Application to Lunar Landing."
Item
Dublin Core
Identifier
Iterguidscheitsappllunaland.pdf
spc_stnv_000348
Title
"An Iterative Guidance Scheme and Its Application to Lunar Landing."
Alternative Title
TN D-2869
Description
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.
Creator
Date
1965-07-01
Temporal Coverage
Source
Saturn V Collection
Box 14, Folder 22
University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
Language
Rights
This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections.
Relation
spc_stnv_000325_000349
Is Referenced By
<a href="http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17169"> View this item in ArchivesSpace. </a>
Collection
Citation
Horn, Helmut J., “"An Iterative Guidance Scheme and Its Application to Lunar Landing.",” UAH Archives, Special Collections, and Digital Initiatives, accessed November 13, 2024, http://libarchstor2.uah.edu/digitalcollections/items/show/10969.