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Block Diagram of Communication System with Detailed Explanation - Electronics Post

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Block Diagrams of Control Systems 1.4

An aircraft's attitude varies in roll, pitch, and yaw as defined in Figure p 1.2 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