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Self-adaptive weighting differential game guidance method

A technology of adaptive weighting and differential countermeasures, applied in the field of aircraft guidance, can solve the problem of no reasonable basis for the determination of the penalty coefficient and conservative guidance laws.

Inactive Publication Date: 2013-01-30
空军工程大学航空航天工程学院
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AI Technical Summary

Problems solved by technology

[0004] The present invention provides an adaptive weighted differential game guidance method, aiming at solving the problem that the currently designed differential game guidance law has no reasonable basis for determining the penalty coefficient of the target control amount, and the current differential game guidance law is based on symmetrical complete state information model, making the designed guidance laws too conservative

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Embodiment Construction

[0051] In order to make the purpose, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the invention.

[0052] figure 1 It shows the implementation process of the adaptive weighted differential game guidance method provided by the present invention.

[0053] The adaptive weighted differential game guidance method includes the following steps:

[0054]A. Obtain Vr, Dr and dq from the relative motion of the aircraft and the target;

[0055] B. Estimating the acceleration of the target through the state filter and estimated error p;

[0056] C. Will Input the first controller, and output the guidance law u for the case of asymmetric incomplete state information 1 ;

[0057] D. Will and p input pa...

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Abstract

The invention belongs to the technical field of air vehicle guidance and provides a self-adaptive weighting differential game guidance method aiming at a high maneuvering target. The method includes deriving a differential game guidance law under the conditions of symmetrical complete information and asymmetrical incomplete information according to different information modes; self-adaptively adjusting a penalty coefficient in a quadratic index according to estimation results of a state filter and a current maneuvering capacity; and finally, switching the different information modes according to estimation errors and self-adaptively changing a pursuit strategy to further form the self-adaptive weighting differential game guidance method. According to the self-adaptive weighting differential game guidance method, state information measured by a sensor is fully utilized, the information modes are timely adjusted according to changes of outside environments, the problems that reasonable evidences for setting target penalty coefficients are absent and ordinary differential game guidance laws are conservative are effectively solved, guidance accuracy of air vehicles is effectively and scientifically improved, and the method has high application values.

Description

technical field [0001] The invention belongs to the technical field of aircraft guidance, in particular to an adaptive weighted differential countermeasure guidance method. Background technique [0002] With the development of aerospace science and technology, aircraft guidance technology has always been the focus of attention of countries all over the world. As the "nerve center" of the aircraft system, the guidance system plays an extremely important role. At present, the threat of various strong maneuvering targets (such as: tactical ballistic missiles, intelligent cruise missiles and intelligent drones, etc.) is becoming more and more prominent, which brings great challenges to the guidance and control systems of aircraft. Differential game theory combines game theory and optimal control theory, and has obvious advantages in describing the dynamic confrontation process. The "chasing and fleeing problem" described in his theory is exactly the problem of differential gam...

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Application Information

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IPC IPC(8): G05D1/10G05B13/04
Inventor 方洋旺张平伍友利张艺瀚李锐
Owner 空军工程大学航空航天工程学院
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