Design a Derivative-Filtered Aircraft Attitude Controller
Random sensor noise may get amplified around a control loop, causing high-frequency "chatter" in the control signal. Minimize the resulting actuator wear with a derivative-filtered controller for an aircraft attitude control system.
The elevator actuator and aircraft models.
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The PID controller.
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The ramp reference-following control action in the presence of sensor noise.
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A derivative-filtered PID controller provides smoother control.