ENG5008 Aerospace Control I 2017
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Aerospace Control I (ENG5008)
2017
SECTION A
Q1 |
(a)
(b) |
Draw a Nyquist plot for a stable closed loop system and for an unstable system. For the stable system, mark the gain margin, phase margin and the vector margin in the plot. Explain the meaning of gain margin, phase margin and vector margin. [5] For a control system with a nominal plant P0 , the Nyquist plot of the loop-gain L shows a phase margin of 60deg at a frequency of 4rad/sec. The plot crosses the negative real axis at -0.8. (i) What additional delay can be added to the closed loop before stability is lost? [3] (ii) By how much can the plant gain increase before the closed loop becomes unstable? [2] |
(c) Given the transfer function
G(s) =
derive the state space description in observer canonical form. [5]
(d) What is meant by the Separation Theorem in the context of state-estimator
feedback control? [5]
Show that for an open-loop structure the ideal compensator should cancel the plant dynamics, and state the drawbacks of this approach. Describe a feedback structure which can provide approximate plant inversion, and show therefore
that high-gain closed-loop control implicitly inverts plant dynamics. [5]
What are the three components of a PID controller? Briefly analyse the advantages and disadvantages of each. In your analysis you should focus on how each component affects the shape of the loop gain, and how this in turn
influences characteristics of the closed loop system. [5]
Explain the concept of “internal stability” and relate this to BIBO stability, using a block-diagram similar to that shown in Figure 1. Why is it important to
Describe a test for controllability of a state space system. [5]
Section B
Describe potential benefits and drawbacks of a closed-loop control strategy and contrast these to an open-loop strategy. In your analysis, focus on the characteristics of each structure with respect to plant disturbances, changes in
the plant gain, and stabilisation. [5]
Consider the closed loop system shown in Figure Q3
(i) Derive the closed-loop equation of this system, and define the loop gain L, the sensitivity function S and the complementary sensitivity function
T . [5]
(ii) Sketch the typical shapes of the frequency responses of the magnitudes
ofL, S, and T. Explain how this is related to characteristics of the closed loop system, in particular how the closed loop behaviour at low
frequencies and at high frequencies is defined by this. [5]
Show that the sensitivity function S0 is equal to the sensitivity of the complementary sensitivity T0 to changes in the plant P0 . By a symmetry argument, briefly describe the effect of T0 on the sensitivity of S0 to plant changes. [5]
Figure Q3
Describe the concept of state feedback control using a block diagram and
derive the differential equation of the closed loop system. [5]
For the state feedback system from (a), what is controller design by pole assignment and how can it be used to design a state feedback controller? [5]
What is controllability in the context of state feedback control and what is meant
by stabilisability? [3]
Consider the system
[2(1)] = [ ] [2(1)] + [0(1)]
1
Show whether this system is controllable or not. [2]
(e) Design a state feedback controller K for the state space system given in (d)
using the pole placement method in such a way that the closed system has an overshoot of Mp=1% and a rise time of tr=0. 1 seconds. You can use the following equations to derive the natural frequency and the damping of the desired closed loop system:
1.8 ln Mp
[5]
2022-08-01