A Thrust Control Method of Solid Rocket Motor Based on Radial Basis Neural Network

A technology based on neural networks and solid rockets, applied in the field of thrust control of solid rocket motors based on radial basis neural networks, can solve problems such as unmodeled dynamic control difficulties, and achieve good tracking ability, good anti-interference and robustness sexual effect

Active Publication Date: 2022-04-05
SHENYANG AEROSPACE UNIVERSITY +1
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Problems solved by technology

In recent years, due to the development of neural networks, many studies have applied radial basis neural networks to the control of dynamic objects, but from the perspective of control methods, it is still the first to use radial basis neural networks for solid rocket control. For rocket engine control, its parameters will change drastically with the environment, and the unmodeled dynamics will also bring certain difficulties to the control, and the radial basis neural network has a good adaptive function, which can better overcome this problem

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  • A Thrust Control Method of Solid Rocket Motor Based on Radial Basis Neural Network
  • A Thrust Control Method of Solid Rocket Motor Based on Radial Basis Neural Network
  • A Thrust Control Method of Solid Rocket Motor Based on Radial Basis Neural Network

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[0047] In order to make the object, technical solution and advantages of the present invention clearer, 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 present invention.

[0048] The technical steps of a radial basis neural network solid rocket motor thrust control technology based on genetic algorithm optimization provided by the present invention are as follows:

[0049] Step 1. Determine the control object. The actuator adopts a gas regulating system and a pneumatic servo system, and selects a solid rocket motor as a power device. The pneumatic servo system includes a high-pressure gas cylinder 1, an on-off valve 2, a pressure reducing valve 3, a control valve 4, and a needle The pneumatic servo system composed of the valve head 8 and the needle valve head chamber...

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Abstract

The invention provides a solid rocket motor thrust control method based on a radial basis neural network, which is characterized in that it includes the following steps: Step 1. Determine the control object, the executive mechanism adopts a gas regulating system and a pneumatic servo system, and selects a solid rocket motor as Power plant; Step 2. Establish the mathematical model of the controlled object of the solid rocket motor; Step 3. Establish the reference model and the actual model according to the expected control performance requirements; Step 4. Design the RBF neural network control for the thrust adaptive control of the solid rocket motor The device selects the learning index of the neural network; Step 5. utilizes the genetic algorithm to optimize the parameters of the RBF neural network controller; the present invention optimizes the parameters of the neural network through the genetic algorithm, so that the solid rocket motor control system based on the RBF neural network is given reference The model characteristics have good tracking ability, and have good anti-interference and robustness.

Description

technical field [0001] The invention relates to the field of automatic control, in particular to a thrust control method of a solid rocket motor based on a radial basis neural network. Background technique [0002] Solid rocket motor, also known as solid propellant rocket motor, uses solid propellant, which can meet the requirements of the new generation of tactical missiles for its power plant to the greatest extent. It has the advantages of small size, light weight, fast speed and good maneuverability. An ideal propulsion system is a strategic weapon that countries give priority to development. [0003] A large number of theories and experiments have been done for the solid rocket motor with controllable thrust at home and abroad. In order to ensure that the solid rocket can fly according to the predetermined orbit, it is necessary to make corresponding guidance and control. The attitude control of the rocket is realized through the thrust vector control system, and the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B13/04G05B11/42G06N3/08F02K9/80
CPCG05B13/042G05B13/027G05B11/42G06N3/086F02K9/805
Inventor 齐义文陈铖李献领刘金福卢少微刘远强喻勇涛
Owner SHENYANG AEROSPACE UNIVERSITY
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