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.
The PID controller.
The ramp reference-following control action in the presence of sensor noise.
A derivative-filtered PID controller provides smoother control.