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]
.png)
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.
Step by Step Solution
3.41 Rating (164 Votes )
There are 3 Steps involved in it
The loop transfer function is We desire dominant roots ... View full answer
Get step-by-step solutions from verified subject matter experts
Document Format (1 attachment)
835-C-S-S-A-D (2064).docx
120 KBs Word File
