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Lu Zhenduo(Beijing Institute of Control Engineering, Beijing 100080)
Published:
Abstract: he paper discusses a general principle of attitude control during orbit maneuver.The attitude control requirements are different for two stabilized modes of a satellite.The paper emphatically analyses key teehnological problems on the control system design of three axis stabilized satellite during orbit maneuver.
Lu Zhenduo(Beijing Institute of Control Engineering, Beijing 100080). ATTITUDE CONTROL DURING ORBIT MANEUVER[J]. .
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