Mission planning for the space maneuver vehicle

被引:0
|
作者
Wiesel, WE [1 ]
机构
[1] USAF, Inst Technol, Dept Aeronaut & Astronaut, Wright Patterson AFB, OH 45433 USA
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中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Mission planning for the Air Force Space Maneuver Vehicle (SMV) requires wholesale solution of the Lambert problem about an oblate earth. We discuss numerical and algorithmic aspects of this solution, as well as the orbital element inverse problem: determining the orbital elements that yield a give position and velocity at a given time.
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页码:2043 / 2049
页数:7
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