A hypersonic aircraft expert intelligent control method and aircraft

A hypersonic, intelligent control technology, applied in the field of aircraft control, can solve problems such as difficulty in adapting to severe aerodynamic changes during aircraft deformation, and difficulty in obtaining control effects in aircraft motion control, and achieve high-precision stable control, intelligent adjustment, and solution. Adjust difficult effects

Active Publication Date: 2022-03-11
NAT UNIV OF DEFENSE TECH
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AI Technical Summary

Problems solved by technology

However, in the current control methods for deformable aircraft, the parameter selection of the controller is usually a set of fixed parameters selected in advance, which brings about the problem that for hypersonic deformable aircraft, a set of controller parameters is difficult to adapt The deformation process of the aircraft and the severe aerodynamic changes at hypersonic speeds make it difficult to obtain the optimal control effect for the motion control of the aircraft

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  • A hypersonic aircraft expert intelligent control method and aircraft
  • A hypersonic aircraft expert intelligent control method and aircraft
  • A hypersonic aircraft expert intelligent control method and aircraft

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Embodiment Construction

[0031] In order to facilitate the implementation of the present invention, further description will be given below in conjunction with specific examples.

[0032] Such as figure 1 Shown is a schematic diagram of the control flow of this embodiment. Before the control flow, an expert system needs to be established. In the expert system, the knowledge base plays a very important role, which will directly determine whether the expert system can run normally. In the expert system, according to the experience of the experts from the system state and performance characteristics, the control law of debugging is summarized, and the rules of setting PID control parameters are described in the expert language, and then stored in the knowledge base.

[0033] In this embodiment, the flight debugging process of the hypersonic vehicle is the experience of experts (expert language), that is, the rate of change of the length of the hypersonic vehicle and the rate of change of the sweep angle ...

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Abstract

The invention provides an expert intelligent control method for a hypersonic vehicle, comprising: constructing an expert system, and pre-establishing a knowledge base of one-to-one correspondence between the real-time deformation state of the hypersonic vehicle and the control parameters of the PID controller in the expert system; The real-time deformation state of the hypersonic vehicle determines the real-time control parameters of the PID controller of the hypersonic vehicle; the PID controller controls the hypersonic vehicle in real time according to the real-time control parameters determined in step S2. An expert system is designed to determine the real-time control parameters of the PID controller of the hypersonic vehicle according to the real-time deformation state of the hypersonic vehicle, which realizes the intelligent adjustment of the control parameters and improves the adaptability of the control parameters, which is suitable for the design of the control system of the hypersonic vehicle , effectively solve the problem of difficult adjustment of hypersonic vehicle controller control parameters. The invention is applied in the field of aircraft control.

Description

technical field [0001] The invention relates to the field of aircraft control, in particular to an expert intelligent control method for a hypersonic aircraft and the aircraft. Background technique [0002] Hypersonic deformable aircraft is a special type of hypersonic aircraft, whose main feature is that it can actively change its shape and structure according to the requirements of the flight environment and flight missions, so as to obtain better aerodynamic characteristics and maneuverability, and achieve wide range with less energy consumption. High speed and wide airspace flight. The hypersonic deformable aircraft takes the shape parameters as controllable variables, and uses the influence of the shape parameters on the aerodynamic characteristics to change the performance of the aircraft, so that it can adapt to a wider range of flight airspace and speed domain, so that it can adapt to more complex flight tasks and flight environment. At the same time, the hypersoni...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 王鹏汤国建
Owner NAT UNIV OF DEFENSE TECH
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