Singular perturbation analysis of AOTV-related trajectory optimization problems
By: Anthony J. Calise.
Contributors: Langley Research Center.; Georgia Institute of Technology. School of Aerospace Engineering.
Series: NASA CR -- 186202.; NASA contractor report -- NASA CR-186202.
Publisher: Georgia Institute of Technology, School of Aerospace Engineering; National Aeronautics and Space Administration, Langley Research Center; For sale by the National Technical Information Service
Published: 1990
Place of publication: Atlanta, GA; [Hampton, VA; Springfield, VA
Language: eng
Format: Microform
Subjects: Aeroassist.; Guidance (Motion); Maneuverable reentry bodies.; Orbit  transfer vehicles.; Perturbation.; Research vehicles.; Trajectories.; Trajectory optimization.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 7/7/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900006620%5F1990006620.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche.