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Shock and Vibration
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Shock and Vibration
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2018
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Article
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Tab 3
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Research Article
Attitude Maneuvering and Vibration Reducing Control of Flexible Spacecraft Subject to Actuator Saturation and Misalignment
Table 3
Steady observation errors of modal observer.
Steady observation errors
Mode 1
7.381
e
− 6
Mode 2
1.61
e
− 7
Mode 3
0
Mode 4
3.92
e
− 7