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Volumn 10, Issue 3, 2006, Pages 222-232
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Overview of some optimal control methods adapted to expendable and reusable launch vehicle trajectories
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Author keywords
Launcher; Optimization; Trajectory
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Indexed keywords
OPTIMIZATION;
PROBLEM SOLVING;
SPACE FLIGHT;
TRAJECTORIES;
OPTIMAL CONTROL;
POLYVALENT;
REUSABLE LAUNCH VEHICLES;
CATAPULTS (AIRCRAFT LAUNCHERS);
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EID: 33646469132
PISSN: 12709638
EISSN: None
Source Type: Journal
DOI: 10.1016/j.ast.2005.11.004 Document Type: Article |
Times cited : (28)
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References (6)
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