The system shown in Figure represents the problem of stabilizing the attitude of a rocket during takeoff or controlling the
MLÎ¸ - (M + m)gÎ¸ = f
Where f is the control variable. Design a control law to maintain Î¸ near zero. The specifications are Î¶ = 0.707 and a 2% settling time of 8 sec. The parameter values are M = 40 slugs, m = 8 slugs, L = 20 ft, and g = 32.2 ft/sec2.
This problem has been solved!
Do you need an answer to a question different from the above? Ask your question!
Step by Step Answer:
Create a free account to access the answer
Cannot find your solution?
Post a FREE question now and get an answer within minutes. * Average response time.
Question Posted: March 17, 2016 03:31:36