文件名称:Attitude-Control-of-Spinning-Satellite
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simulate multivariable system control.
Attitude Control of Spinning Satellite Subject to Actuators
Restriction Using EigenStructure Assignment.
Attitude Control of Spinning Satellite Subject to Actuators
Restriction Using EigenStructure Assignment.
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Attitude Control of Spinning Satellite\Attitude Control of Spinning Satellite.m
......................................\Attitude Control of Spinning Satellite.pdf
Attitude Control of Spinning Satellite
......................................\Attitude Control of Spinning Satellite.pdf
Attitude Control of Spinning Satellite