Question

A position control system converts a position input command to a position output response. Position control systems find widespread applications in antennas, robot arms, computer disk drives, and the radio telescope antenna. The aircraft's attitude in Figure is one example of a system that uses position control systems. An aircraft's attitude varies in roll, pitch, and yaw as defined in Figure. Draw a functional block diagram for a closed-loop system that stabilizes the roll as follows: The system measures the actual roll angle with a gyro and compares the actual roll angle with the desired roll angle. The ailerons respond to the roll-angle error by undergoing an angular deflection. The aircraft responds to this angular deflection, producing a roll angle rate. Identify the input and output transducers, the controller, and the plant. Further, identify the nature of each signal. y Pitch angle Aileron deflection up Aileron deflection down Roll angle x Yaw angle z Each student has to read about that closed-loop application and to submit a word file including the following: 1. Cover page (Title of the application, Student's name, course code, semester, and Effat logo) 2. Outline (table of contents) 3. Problem statement 4. For solving the problem: sketch diagrams to explain the system concept, detailed layout, and schematic. 1. Conclusion 2. References 3. Your report maybe in the range of 10 pages.

          A position control system converts a position input command to a position output response. Position control
systems find widespread applications in antennas, robot arms, computer disk drives, and the radio telescope
antenna. The aircraft's attitude in Figure is one example of a system that uses position control systems.
An aircraft's attitude varies in roll, pitch, and yaw as defined in Figure. Draw a functional block diagram
for a closed-loop system that stabilizes the roll as follows:
The system measures the actual roll angle with a gyro and compares the actual roll angle with the desired roll
angle. The ailerons respond to the roll-angle error by undergoing an angular deflection. The aircraft responds
to this angular deflection, producing a roll angle rate. Identify the input and output transducers, the controller,
and the plant. Further, identify the nature of each signal.
y
Pitch angle
Aileron
deflection up
Aileron
deflection down
Roll angle
x
Yaw angle
z
Each student has to read about that closed-loop application and to submit a word file including the following:
1. Cover page (Title of the application, Student's name, course code, semester, and Effat logo)
2. Outline (table of contents)
3. Problem statement
4. For solving the problem: sketch diagrams to explain the system concept, detailed layout, and schematic.
1. Conclusion
2. References
3. Your report maybe in the range of 10 pages.

Added by Amy G.

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