Question: The attitude control system of a space shuttle rocket is shown in Figure DP6.4 [17]. (a) Determine the range of gain K and parameter m

The attitude control system of a space shuttle rocket is shown in Figure DP6.4 [17].
(a) Determine the range of gain K and parameter m so that the system is stable, and plot the region of stability.
(b) Select the gain and parameter values so that the steady-state error to a ramp input is less than or equal to 10% of the input magnitude.
(c) Determine the percent overshoot for a step input for the design selected in part (b).
Figure DP6.4
Shuttle attitude control.

The attitude control system of a space shuttle rocket is

Space shuttle rocket Controller Ris) Attitude

Step by Step Solution

3.40 Rating (169 Votes )

There are 3 Steps involved in it

1 Expert Approved Answer
Step: 1 Unlock

a The closedloop characteristic polynomial is s 3 K... View full answer

blur-text-image
Question Has Been Solved by an Expert!

Get step-by-step solutions from verified subject matter experts

Step: 2 Unlock
Step: 3 Unlock

Document Format (1 attachment)

Word file Icon

835-C-S-S-A-D (1744).docx

120 KBs Word File

Students Have Also Explored These Related Systems Analysis And Design Questions!