Optimal guidance law develpment for an advanced launch system
By: Anthony J. Calise and Martin S.K. Leung.
Contributors: Leung, Martin S. K.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-4667.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Advanced launch system (STS); Algorithms.; Ascent trajectories.; Injection guidance.; Launch vehicles.; Optimal control.; Perturbation theory.; Problem solving.; Real time operation.; Spacecraft guidance.; Trajectory optimization.; Transearth injection.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0615-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 2 microfiches.