Overview of some optimal control methods adapted to expendable and reusable launch vehicle trajectories
- 30 April 2006
- journal article
- Published by Elsevier BV in Aerospace Science and Technology
- Vol. 10 (3), 222-232
- https://doi.org/10.1016/j.ast.2005.11.004
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- FLOP: ONERA's Answer to Trajectory Optimization for Future LaunchersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2003
- Survey of Numerical Methods for Trajectory OptimizationJournal of Guidance, Control, and Dynamics, 1998