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Hypersonic aircraft airborne trajectory planning method and device, aircraft and medium

A hypersonic and trajectory planning technology, applied in the field of aircraft control, achieves the effect of great significance, guaranteed real-time performance, and real-time airborne high-precision trajectory planning capabilities

Pending Publication Date: 2022-03-29
NAT UNIV OF DEFENSE TECH
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AI Technical Summary

Problems solved by technology

[0005] Aiming at the trajectory planning problem of hypersonic vehicle reentry gliding section in the prior art, the object of the present invention is to provide a hypersonic vehicle airborne trajectory planning method, device, aircraft and medium

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  • Hypersonic aircraft airborne trajectory planning method and device, aircraft and medium
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  • Hypersonic aircraft airborne trajectory planning method and device, aircraft and medium

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Embodiment Construction

[0033] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the spirit of the disclosure of the present invention will be clearly described below with the accompanying drawings and detailed descriptions. Any person skilled in the art will understand the embodiments of the present invention. , when it can be changed and modified by the technology taught in the content of the present invention, it does not depart from the spirit and scope of the content of the present invention. The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not to limit the present invention.

[0034] refer to figure 1 , in one embodiment of the present invention, a hypersonic vehicle airborne trajectory planning method is provided, including:

[0035] The motion equation of the hypersonic vehicle's re-entry glide phase is used as the training environment for the trajectory plann...

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Abstract

The invention discloses a hypersonic aircraft airborne trajectory planning method and device, an aircraft and a medium. A reentry gliding section motion equation of a hypersonic aircraft is used as a training environment of a trajectory planning problem of the hypersonic aircraft; constructing a state space, a strategy action space, an environment dynamic transfer function, a reward function and a discount factor of the trajectory planning problem; and training the neural network of the trajectory planning problem by using a deep reinforcement learning algorithm. And inputting the state space obtained in the flight process into the trained Actor network to obtain a strategy action space, so that the hypersonic aircraft flies to a predetermined target area according to the strategy action space to complete the flight task of reentering the gliding section. According to the method, airborne real-time trajectory planning of the hypersonic flight vehicle in the gliding section is realized by using an artificial intelligence algorithm, the task adaptability of the flight vehicle is improved, and the problem that the trajectory of the hypersonic deformation flight vehicle like gliding flight is difficult to plan on line is effectively solved.

Description

technical field [0001] The invention belongs to the technical field of aircraft control, and in particular relates to a hypersonic aircraft airborne trajectory planning method, device, aircraft and medium. Background technique [0002] The online trajectory generation task of the hypersonic gliding vehicle’s re-entry gliding segment is to output instructions in real time to guide the vehicle from the current Fly to the preset target area precisely. The trajectory effect of the gliding section not only determines whether the aircraft can fly to the target area, but also affects the flight status of the starting point of the dive section. In traditional aircraft trajectory planning, it is assumed that the initial state of the aircraft is known, and the optimal trajectory is obtained in advance. However, in the actual flight of hypersonic glide, due to flight uncertainty and external interference, this assumption is difficult to establish, which means that the initial state o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 王鹏鲍存余何睿智汤国建
Owner NAT UNIV OF DEFENSE TECH
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