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Figure 4-55.is a block diagram of a space-vehicle at- titude control system. Assuming the time constant T of the controller to be 3 sec
Figure 4-55.is a block diagram of a space-vehicle at- titude control system. Assuming the time constant T of the controller to be 3 sec and the ratio of torque to inertia KIJ to berad/sec?, find the damping ratio of the system. R(s) K(Ts + 1) Js Space vehicle
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Process Dynamics And Control
Authors: Dale E. Seborg, Thomas F. Edgar, Duncan A. Mellich
2nd Edition
471000779, 978-0471000778
