A steady state compensator of specified order is proposed to estimate the required duty cycle needed to balance the distribution torque. The compensator was increased gradually to demonstrate the improvement in pointing accuracy. The basic mathematical model of the flexible spacecraft and sensor used to characterize the performance of the compensator are described.
Spacecraft attitude pointing performance during orbit adjust as a function of compensator order
1981-10-01
Conference paper
No indication
English
Attitude pointing schemes and spacecraft configurations for libration-point-orbit spacecraft
Online Contents | 2017
|Attitude pointing schemes and spacecraft configurations for libration-point-orbit spacecraft
Online Contents | 2017
|British Library Conference Proceedings | 2000
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