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2003•Journal of Projectiles.Rockets.Missiles and GuidanceRequires access

The Optimal Guidance Law for Attacking Maneuvering Targets

Hongke Wang

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Abstract

By setting up the simplified mathematic model of the air-to-air missile attacking maneuvering targets. Based on the model,the state equation and the measurement equation are proposed.Considering the maneuvering target and delay of the missile,by utilizing the design method of the Lianear Quadratic.Regulator and the Kalman filter theory,a new optimal guidance law and filter formulation for infrared and radar homing missile are put forward, which has good adaptability and high precision for attacking maneuvering targets.

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What this paper is about

By setting up the simplified mathematic model of the air-to-air missile attacking maneuvering targets. Based on the model,the state equation and the measurement equation are proposed.Considering the maneuvering target and delay of the missile,by utilizing the design method of the Lianear Quadratic.Regulator and the Kalman filter theory,a new optimal guidance law and filter formulation for infrared and radar homing missile are put forward, which has good adaptability and high precision for attacking maneuvering targets.

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Available abstract

By setting up the simplified mathematic model of the air-to-air missile attacking maneuvering targets. Based on the model,the state equation and the measurement equation are proposed.Considering the maneuvering target and delay of the missile,by utilizing the design method of the Lianear Quadratic.Regulator and the Kalman filter theory,a new optimal guidance law and filter formulation for infrared and radar homing missile are put forward, which has good adaptability and high precision for attacking maneuvering targets.

Key concepts: Missile, Missile guidance, Kalman filter, Control theory (sociology), Air-to-air missile, Adaptability, Proportional navigation, Computer science

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