2011Journal of Sichuan OrdnanceRequires access

Establishment of Proportional Guidance Trajectory Based on Guidance Principle

Rui Zhang

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Abstract

The paper researched on the calculation error of proportional guidance method widely used at present.After analyzing the principle of self-guidance part,the trajectory function was established,and it simulated the two-dimensional problem.Finally it concluded the relationship between proportional guidance quotient and the velocity ratio of aircraft and target.Comparison with the R-K method,the improved algorithm is more accurate.

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What this paper is about

The paper researched on the calculation error of proportional guidance method widely used at present.After analyzing the principle of self-guidance part,the trajectory function was established,and it simulated the two-dimensional problem.Finally it concluded the relationship between proportional guidance quotient and the velocity ratio of aircraft and target.Comparison with the R-K method,the improved algorithm is more accurate.

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Available abstract

The paper researched on the calculation error of proportional guidance method widely used at present.After analyzing the principle of self-guidance part,the trajectory function was established,and it simulated the two-dimensional problem.Finally it concluded the relationship between proportional guidance quotient and the velocity ratio of aircraft and target.Comparison with the R-K method,the improved algorithm is more accurate.

Key concepts: Trajectory, Control theory (sociology), Quotient, Proportional navigation, Function (biology), Computer science, Mathematics, Engineering

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