[PDF] Automated Controller Design for a Missile Using Convex Optimization

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Automated Controller Design for a Missile Using Convex Optimization

Abstract:

The focus of the present master thesis is the automation of an existing controller design for a missile using two aerodynamic actuating systems. The motivation is to evaluate more missile concepts in a shorter period of time. The option used is trimming and linearization of a highly nonlinear missile at special conditions. According to these conditions, either a two-dimensional operating point grid de ned by Mach number and height or three-dimensional operating point grid de ned by Mach number, height and angle of attack is generated for the whole operating range of the missile.

The whole design was successfully developed and tested in MATLAB/Simulink on missiles using one or two aerodynamic actuating systems. The controllers have a good performance at small and high acceleration steps and the anti-windup keeps the missile stable even though the actuators are saturated. Stability and robustness of the controllers and anti-windup networks was veri ed as well as an air defense maneuver where the missile starts at the ground and intercepts a target at high altitude was successfully simulated for di erent grids and missiles.

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