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Guidance Law Design and Simulation for Television Guided Micro Missile

LI Chun-ke

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Abstract

In order to adapt to the developmental trend of micro missiles,guidance design for the ground-launched,television-guided micro missiles is investigated.In terms of a certain model of high-precision micro-missiles,motion equations of missile in the vertical plane are established.The compound guidance,in which the initial guidance is program guidance and the terminal guidance is proportion guidance,is designed by the working principle of TV seeker.Based on the MATLAB/Simulink simulation platform,simulation model is established under modular modeling idea.The simulation results validate the feasibility of the guidance law and guidance accuracy.

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What this paper is about

In order to adapt to the developmental trend of micro missiles,guidance design for the ground-launched,television-guided micro missiles is investigated.In terms of a certain model of high-precision micro-missiles,motion equations of missile in the vertical plane are established.The compound guidance,in which the initial guidance is program guidance and the terminal guidance is proportion guidance,is designed by the working principle of TV seeker.Based on the MATLAB/Simulink simulation platform,simulation model is established under modular modeling idea.The simulation results validate the feasibility of the guidance law and guidance accuracy.

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Available abstract

In order to adapt to the developmental trend of micro missiles,guidance design for the ground-launched,television-guided micro missiles is investigated.In terms of a certain model of high-precision micro-missiles,motion equations of missile in the vertical plane are established.The compound guidance,in which the initial guidance is program guidance and the terminal guidance is proportion guidance,is designed by the working principle of TV seeker.Based on the MATLAB/Simulink simulation platform,simulation model is established under modular modeling idea.The simulation results validate the feasibility of the guidance law and guidance accuracy.

Key concepts: Missile, Missile guidance, Guidance system, Terminal guidance, Modular design, MATLAB, Simulation, Computer science

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