2008
DOI: 10.1299/kikaic.74.2698
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Steering Law of Control Moment Gyros Using Optimization of Initial Gimbal Angles for Satellite Attitude Control

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Cited by 7 publications
(2 citation statements)
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“…The law can avoid singularity to a certain extent, but the effect of escaping singularity is not ideal. In 2010, Takada et al [5] proposed the CMG singularity avoidance control law based on a singular surface cost function, which avoids the internal singularity of the system by introducing torque error. In 2011, Nanamori et al [6] proposed a new optimal initial frame angle control law without knowing the trajectory of the desired torque in advance.…”
Section: Introductionmentioning
confidence: 99%
“…The law can avoid singularity to a certain extent, but the effect of escaping singularity is not ideal. In 2010, Takada et al [5] proposed the CMG singularity avoidance control law based on a singular surface cost function, which avoids the internal singularity of the system by introducing torque error. In 2011, Nanamori et al [6] proposed a new optimal initial frame angle control law without knowing the trajectory of the desired torque in advance.…”
Section: Introductionmentioning
confidence: 99%
“…Applying the propesed method reduces the probability of failure of the CMG at the end stage of the design lifetime. In more detai1, the proposed steering law levels the gimbal angle displacements of four CMGs in a pyrarnid eonfiguration, and keeps the manipulability greater by utilizing the dependence of each gimbal motion of the CMG on a set ofinitial gimbal angles (Nanamori and Takahashi, 2008). The proposed method changes the set ofinitial gimbal angles by inserting null motion between maneuvers; i.e., it changes the steering path in the angular momentum space of the CMGs subsequently,…”
Section: Introductionmentioning
confidence: 99%