An online intelligent planning method for missile track

A technology of intelligent planning and trajectory planning, which is applied in the field of aircraft control, can solve the problems of real-time planning trajectory, reliability cannot be well guaranteed, and missile trajectory planning cannot be achieved, so as to avoid the disadvantage of easily falling into local minimum and improve The effect of operating efficiency

Active Publication Date: 2022-07-22
JIANGSU UNIV
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AI Technical Summary

Problems solved by technology

[0011] (1) Most of them can only solve the trajectory planning problem of known static / slow obstacles existing in the environment;
[0012] (2) The real-time performance and reliability of the planned trajectory cannot be well guaranteed, resulting in the inability to be directly applied to missile trajectory planning in complex combat environments

Method used

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  • An online intelligent planning method for missile track

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Embodiment Construction

[0036] In order to make the objectives, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.

[0037] like figure 1 A method for online intelligent planning of missile track is shown, including the following steps:

[0038]Step 1, in order to avoid the APF method, when the moving body and the target are relatively close, this algorithm is easy to fall into the local optimum, resulting in the inability to plan the track, and considering that in the initial stage of the terminal guidance, the missile is far away from the target. Based on this, the present invention plans to use the offline and online APF method to plan the missile track at this stage; and train the A3C network to obt...

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Abstract

The invention discloses an online intelligent planning method for missile tracks, which combines the traditional track planning method APF and the new generation artificial intelligence method A3C represented by deep reinforcement learning. It is easy to fall into the local minimum shortcomings, and it can effectively solve the problem of slow network convergence in artificial intelligence methods. The algorithm to be established is as follows: in the initial stage of terminal guidance, use the offline and online APF method to plan the missile track, and at the same time, use the generated track to train the A3C network "underground" to obtain stable network parameters. Since the track accuracy of the APF method at this stage is much higher than that obtained by the A3C algorithm, it can greatly speed up the network training speed and improve the efficiency of the algorithm. When the A3C network parameters are stable, a two-stage fast switching method is proposed to make the algorithm switch from APF to A3C autonomously and quickly, and the network-stabilized A3C algorithm is used to provide the missile suboptimal / optimal planning track.

Description

technical field [0001] The invention belongs to the field of aircraft control, and in particular relates to an online intelligent planning method for an aircraft track. Background technique [0002] In recent years, the continuous development of missile technology in various countries has greatly improved the reliability, effectiveness, and precision strike capabilities of missiles. In addition, with the widespread application and integration of technologies such as artificial intelligence, cloud computing, and big data, new technologies continue to flow into the military field, making warfare develop rapidly in the direction of intelligence. It can be seen that the performance and intelligence level of my country's missiles need to be improved urgently. Among them, missile trajectory planning is one of the key technologies that needs to be improved. Missile trajectory planning refers to finding a feasible and optimal trajectory from the starting point to the target point ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
CPCG05D1/107
Inventor 李红霞
Owner JIANGSU UNIV
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