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Shock and Vibration
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Shock and Vibration
/
2018
/
Article
/
Tab 2
/
Research Article
Attitude Maneuvering and Vibration Reducing Control of Flexible Spacecraft Subject to Actuator Saturation and Misalignment
Table 2
Design parameters for the different controllers.
Control schemes
Parameters and values
Proposed controller in (
77
) and (
78
)
Proposed controller in (
54
) and (
55
)