Heat
Autor: Vincent Yu • May 27, 2016 • Research Paper • 812 Words (4 Pages) • 829 Views
Auto Control l – Lab Part A Report
Hongzhi Yu a1657200
INTRODUCTION
Use Matlab and Simulink to study the modelling facilities; the poles and zeros of open loop transfer function; the time response of control systems.
RESULTS
The open-loop transfer function is:
Gol= 62.36
-----------------------------------------
Continuous-time transfer function is:
S^3+11.75s^2+17.55s
The poles are: 0, -10.0000, and -1.7548.
There are no zeros.
The closed-loop transfer function is:
62.36
--------------------------------------------
Continuous-time transfer function is:
S^3+11.75s^2+17.55s+62.36
The poles are: -10.6573, -0.5488+2.3560i, and -0.5488-2.3560i
There are no zeros.
DISCUSSION
The follow steps shows the explanation of the task.
Step 1: Clear any existing variables in memory.
Step 2: Input all conditions and constants.
Step 3: Display the open-loop transfer function and the open-loop poles and zeros.
Step 4: Calculate the closed-loop transfer function with unity proportional gain and feedback.
Step 5: Show the values of open-loop poles and zero.
Step 6: The closed-loop poles and zeros figure-1.
[pic 1]
Fig.1
Step 7: The closed-loop step response figure-2.
[pic 2]
Fig.2
Step 8: Vary the proportional gain (K) from 0.1 to 1.0 in 0.1 increments (Table-1). Show in figure-3.
Choose the value gain (K)= 0.2 because the rise time is short and the peak response is low which means the airplane can rise in short time and keep stable will flying.
[pic 3]
Table 1
[pic 4]
Fig.3
Step 9: Build a Simulink model of the plane roll control system figure-4.
[pic 5]
Fig.4
Step 10: Run the Simulink model and compare the scope results figure-5.
[pic 6]
Fig.5
As show in Fig.5, the diagram of Y(s) is similar to the closed-loop diagram in Fig.3. Start from 0 and constant at 1. The different is the diagram between 0 second and 1 second.
...