Control

The control subsystem translates guidance commands into actuator commands to control the missile’s motion.

Overview

Control systems must:

• Track commanded accelerations or attitudes
• Maintain stability
• Handle aerodynamic uncertainties
• Respond to disturbances

Common control approaches:

• PID control
• LQR (Linear Quadratic Regulator)
• Model Predictive Control
• Adaptive control

Feedback Control Loop

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