The Use of Nonsingular Orbit Elements in Trajectory Optimization in Terms of True Longitude
Conference, Astrodynamics 1995 ; 1995 ; Halifax; Canada
01.01.1996
22 pages
2; pts
Aufsatz (Konferenz)
Englisch
astrodynamics , AIAA , AAS , aeronautics , astronautics
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Trajectory Optimization Using Nonsingular Orbital Elements and True Longitude
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