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A Parameter-Variable Integrated Guidance Law Against Big Maneuvering Target

Yunan Hu

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Abstract

An integrated guidance law combining the proportional navigation and variable structure guidance laws is proposed against big maneuvering target in this paper.Certainly,the structure of the integrated guidance law is simple.The designed mechanism is explained and the variable parameters are optimized.The simulation results show that the missile can effectively intercept the target in a fixed time.

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What this paper is about

An integrated guidance law combining the proportional navigation and variable structure guidance laws is proposed against big maneuvering target in this paper.Certainly,the structure of the integrated guidance law is simple.The designed mechanism is explained and the variable parameters are optimized.The simulation results show that the missile can effectively intercept the target in a fixed time.

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Available abstract

An integrated guidance law combining the proportional navigation and variable structure guidance laws is proposed against big maneuvering target in this paper.Certainly,the structure of the integrated guidance law is simple.The designed mechanism is explained and the variable parameters are optimized.The simulation results show that the missile can effectively intercept the target in a fixed time.

Key concepts: Variable (mathematics), Missile, Proportional navigation, Control theory (sociology), Missile guidance, Simple (philosophy), Law, Guidance system

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