Back to Results
First PageMeta Content
Systems theory / Science / Input shaping / Torque / Vibration / Feedback / Bang–bang control / Control theory / Cybernetics / Physics


Method of Slewing the Spacecraft to Minimize Settling Time
Add to Reading List

Document Date: 2013-06-21 18:13:17


Open Document

File Size: 323,68 KB

Share Result on Facebook

City

Monterey / Washington / D. C. / /

Company

Mathworks Inc. / Distributed Parameter Systems / Buck N. V. / Aeronautics and Astronautics Inc. / /

IndustryTerm

cold gas thrusters / minimum-time solutions / vibratory systems / minimum-time optimal control solution / control law / /

MusicGroup

Ph.D. / National / /

Organization

Congress / Spacecraft Research and Design Center / Flexible Spacecraft Simulator FSS / American Institute of Aeronautics and Astronautics / Naval Postgraduate School / /

Person

Prince / Hong-Jen Chen / /

Position

author / first author / Professor and Director / Feedback Torque PID Controller / Singer / PID controller / controller / /

ProgrammingLanguage

C / MATLAB / /

ProvinceOrState

North Carolina / California / /

Technology

simulation / /

SocialTag