Maneuver device for artificial satellite
作者： Toshiaki Yamashita
DOI:
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摘要: The present invention provides a maneuver device for an artificial satellite, which causes small attitude error during and requires shorter period of setting time obtaining target attitude. is provided with: feed forward torque instruction signal generator 8 outputs 11 based on plan; thruster 10 control the ; calculator 6 to angle angular velocity satellite as well are input 13. further with disturbance compensating detected 16 input, generates 12. yet reaction wheel 7 13
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