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The transfer function for the pitch angle (a) vs gimbal deflection (6) at a particular flight condition is given as a(s) 8(s) = 0.634(s
The transfer function for the pitch angle (a) vs gimbal deflection (6) at a particular flight condition is given as a(s) 8(s) = 0.634(s +0.1534) (s+0.3434) (s-0.1287) (s+0.1543) 1. Is the system stable? Why or why not? 2. Obtain the differential equation for the system. 3. Obtain the state-space representation for the system.
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Modern Control Systems
Authors: Richard C. Dorf, Robert H. Bishop
12th edition
136024580, 978-0136024583
