Study on the Attitude Control of Spacecraft Using Reaction Wheels

Details Study on the Attitude Control of Spacecraft Using Reaction Wheels Study on the Attitude Control of Spacecraft Using Reaction Wheels

Jun 1998

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1998jass...15..245d&link_type=abstract

Journal of Astronomy and Space Sciences, vol. 15, no. 1, p. 245-250.

Astronomy and Astrophysics

Astronomy

Scientific paper

Attitude determination and control of satellite is important component which determines the accomplish satellite missions. In this study, attitude control using reaction wheels and momentum dumping of wheels are considered. Attitude control law is designed by Sliding control and LQR. Attitude maneuver control law is obtained by Shooting method. Wheels momentum dumping control law is designed by Bang-Bang control. Four reaction wheels are configurated for minimized the electric power consumption. Wheels control torque and magnetic moment of magnetic torquer are limited.

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