Trajectory optimization for an asymmetric launch vehicle
By: by Jeanne Marie Sullivan.
Contributors: Massachusetts Institute of Technology.; Charles Stark Draper Laboratory.; United States. National Aeronautics and Space Administration.
Series: NASA CR -- 185630.; NASA contractor report -- NASA CR-185630.
Publisher: Massachusetts Institute of Technolgy; Charles Stark Draper Laboratory, Inc.; National Aeronautics and Space Administration
Published: 1990
Place of publication: [Cambridge, Mass.]; [Washington, D.C
Language: eng
Format: Microform
Subjects: Advanced launch system (STS); Asymmetry.; Conjugate gradient method.; Finite difference theory.; Launch vehicles.; Spacecraft launching.; Trajectory optimization.
Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 2 microfiches.