Optimal guidance law development for an advanced launch system
Subtitle: interim progress report
By: principal investigators: Anthony J. Calise & Dewey H. Hodges.
Contributors: Hodges, Dewey H.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-187652.
Publisher: Georgia Institute of Technology, School of Aerospace Engineering; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1990
Place of publication: Atlanta, GA; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Feedback control.; Finite element method.; Launch vehicles.; Optimal control.; Perturbation theory.; Spacecraft control.; Spacecraft guidance.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.