Question: A simplified version of the attitude rate control for the F-94 or X-15 type aircraft is shown in Figure PI0.3. When the vehicle is flying

A simplified version of the attitude rate control for the F-94 or X-15 type aircraft is shown in Figure PI0.3. When the vehicle is flying at four times the speed of sound (Mach 4) at an altitude of 100,000 ft, the parameters are [26]

A simplified version of the attitude rate control for the

Design a compensator Gc(s) so that the response to a step input has an overshoot of less than 5% and a settling time (with a 2% criterion) of less than 5 seconds.

1 = 1.0 K, = 1.0, = 1.0, and . = 4.

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