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Air countermeasure maneuver control method based on random neural network

A stochastic neural network and mechanism technology, applied in the field of machine learning, can solve the problems of poor migration, poor performance, and high sample complexity, achieve the effect of good maneuver control and improve the ability of migration and generalization

Pending Publication Date: 2021-11-26
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Traditional exploration methods often perform poorly on this task, exhibiting high sample complexity
There are usually two ways to solve the problem of sparse rewards: one is to layer actions, and combine low-dimensional actions into high-dimensional meta-actions to reduce the search space, but requires more domain knowledge and careful design; the other is to use the intrinsic Rewards guide agent exploration without domain knowledge, but poor transferability

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  • Air countermeasure maneuver control method based on random neural network
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  • Air countermeasure maneuver control method based on random neural network

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Embodiment Construction

[0024] In order to make the objectives, technical solutions and advantages of the implementation of the application clearer, the technical solutions in the implementation modes of the application will be described in more detail below with reference to the drawings in the implementation modes of the application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the present application. The embodiments described below by referring to the figures are exemplary and are intended to explain the present application, and should not be construed as limiting the present application. Based on the implementation manners in this application, all other implementation manners obtained by persons of ordinary skill in the art without creative efforts fall within the scope of protection of this application. Embodiments of the pr...

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Abstract

The invention relates to the technical field of machine learning, in particular to an air countermeasure maneuver control method based on a random neural network. The method comprises the following steps: S1, executing a fighter maneuver decision based on a constructed vacuum confrontation model, interacting with a simulation environment, and collecting training sample data; S2, fusing environment external rewards and decision internal rewards to reconstruct a reward mechanism; and S3, training the air confrontation maneuver control method according to the collected training sample data and the reconstructed reward mechanism. Based on the air countermeasure maneuver control method, a fighter can achieve a good maneuvering control effect in an air countermeasure scene, and the migration generalization ability of an algorithm is improved.

Description

technical field [0001] The present application relates to the technical field of machine learning, in particular to an air counter maneuver control method based on a stochastic neural network. Background technique [0002] In the field of air confrontation, smart maneuver control method is the key to defeating the enemy. In the traditional research on fighter maneuver control, most of them are based on the existing maneuver control theory to strengthen the simulation and debugging of the fighter model. This type of maneuver depends to a large extent on the fidelity of the fighter model and human's prior knowledge of maneuver theory, and its flexibility and controllability are poor. With the continuous deepening of artificial intelligence research, fighter maneuver control is also developing towards a more intelligent direction. Among them, reinforcement learning can enable the agent to learn the strategy of obtaining the maximum reward during the interaction with the enviro...

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Application Information

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IPC IPC(8): G06F30/20G06N3/04G05D1/12
CPCG05D1/12G06F30/20G06N3/04
Inventor 韩玥朴海音孙智孝杨晟琦彭宣淇孙阳樊松源于津王鹤卢长谦
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA