Back to Results
First PageMeta Content
Classical mechanics / Mathematical optimization / Lagrange multiplier / Inverse dynamics / Optimal control / Holonomic / Equations of motion / Control theory / Constraint algorithm / Physics / Mathematics / Mathematical analysis


CATION OF CONST AINT DYNAMICS FOR SPACECRAFT MANEUVER Hyochoong Bang and Brij N. Agrawal Naval Postgraduate School, CA[removed]stability problem. For spacecraft , especially flexible spacecraft maneuver, this approach can
Add to Reading List

Document Date: 2009-05-29 17:39:14


Open Document

File Size: 458,67 KB

Share Result on Facebook

City

Amsterdam / Dissertation / Blacksburg / /

Company

Thomson / Distributed Parameter Systems / Aeronautics and Astronautics Inc. / /

Country

Netherlands / /

Facility

American Institute of Aeronautics / Virginia Polytechnic Institute / State University / /

IndustryTerm

inverse dynamics solution / Analytical solution / open control law / possible solution / control law design approaches / control device / error energy / actual control law / control law corresponding / control law / /

Organization

American Institute of Aeronautics and Astronautics / Department of Aeronautics/Astronautics / Naval Postgraduate School / Polytechnic Institute / /

Person

Gq / Lyapunov / /

Position

Assistant Professor / Professor / candidate / /

ProvinceOrState

Virginia / California / /

Technology

Simulation / /

SocialTag