论文信息 - Missile flight control with dynamic inversion and structured singular value synthesis

Missile flight control with dynamic inversion and structured singular value synthesis

An integrated methodology incorporating both dynamic inversion and structured singular value synthesis is employed to design a robust nonlinear autopilot for an air-to-air missile. The nonlinear control elements include nested fast and slow inversion loops which, when closed in the absence of modeling errors, yield a system which is approximately linear. A feedback control law is then designed for this closed-loop system in the presence of structured uncertainties. The current controller architecture addresses those uncertainties and modeling errors which pertain to the fast dynamics.

Christopher D'Souza | Michael McFarland

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