Guidance equations for orbital operations; development of mathematical formulations of maneuver in orbit problem and solutions that can be utilized in analysis of space missions and associated guidance process; factors affecting vehicle motion are isolated and optimum sequence of events required to produce desired motion is defined.
Guidance, flight mechanics and trajectory optimization -- 11
NASA CR
NASA Contractor Reports ; n 1010
1968
117 pages
Report
English
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Guidance, flight mechanics and trajectory optimization -- 16
Engineering Index Backfile | 1968
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Engineering Index Backfile | 1968
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Engineering Index Backfile | 1968
|Guidance, flight mechanics and trajectory optimization -- 17
Engineering Index Backfile | 1968
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Engineering Index Backfile | 1968
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