Optimal Impulsive Rendezvous With Terminal Tangent Burn Between Elliptic and Hyperbolic Orbits Considering the Trajectory Constraints (AAS 14-266)
24th, Spaceflight mechanics meeting ; 2014 ; Santa Fe, NM
2014-01-01
18 pages
Accompanying disc contains complete text in PDF format. Includes bibliographical references and indexes.
Aufsatz (Konferenz)
Englisch
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Optimal two-impulse rendezvous with terminal tangent burn considering the trajectory constraints
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Engineering Index Backfile | 1968
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