Attitude Control of Geostationary Satellite by Using Sliding Mode Control

Details Attitude Control of Geostationary Satellite by Using Sliding Mode Control Attitude Control of Geostationary Satellite by Using Sliding Mode Control

Dec 1996

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1996jass...13..168l&link_type=abstract

Journal of Astronomy and Space Sciences, vol. 13, no. 2, p. 168-173.

Astronomy and Astrophysics

Astronomy

Scientific paper

Magnetic torquer attitude control of a spacecraft by using sliding mode control scheme is considered. Attitude controls to stabilize roll and yaw angles using a magnetic torquer switching control are obtained. Full nonlinear equations of motion for a rigid body spacecraft with constant speed momentum wheel and magnetic torquer are linearized with respect to its equilibrium point, which is normal operating point. Equations for roll and yaw motion are decoupled from those for pitch motion. The feasibility of control law by sliding mode control is demonstrated.

Affiliated with

Also associated with

No associations

Rating

Attitude Control of Geostationary Satellite by Using Sliding Mode Control does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Attitude Control of Geostationary Satellite by Using Sliding Mode Control, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Attitude Control of Geostationary Satellite by Using Sliding Mode Control will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1502552