Self-adaptive high-order sliding mode control method of high-altitude platform air inlet environment simulation system

CN120195997AInactive Publication Date: 2025-06-24SOUTHWEAT UNIV OF SCI & TECH
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Patent Information

Application Number
CN202510671950.5
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-05-23
Publication Date
2025-06-24
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

Due to the complex internal airflow conditions and high uncertainty of the high-altitude platform air intake environment simulation system, it is difficult to maintain accurate tracking of the intake pressure value when the engine throttle lever is operating quickly.

Method used

Adaptive high-order sliding mode control method is adopted, and the adaptive high-order sliding mode controller is designed to control the system by establishing a dynamic second-order model, building an error tracking model, designing integral terminal sliding mode functions and adaptive gain and law.

Benefits of technology

The vibration phenomenon of sliding mode control is reduced, the system's response speed and immunity are improved, the stability and accuracy of the control system are significantly improved, and better smoothness and robustness can be achieved in nonlinear systems with uncertainty.

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Abstract

The invention discloses a self-adaptive high-order sliding mode control method of a high-altitude platform air inlet environment simulation system, and relates to the field of high-altitude platform air inlet environment simulation system control. The method comprises the following steps: establishing a dynamic second-order model of a high-altitude platform air inlet environment simulation system; constructing an error tracking model of the controller; designing a self-adaptive gain and a self-adaptive law of the controller by using an integral terminal sliding mode function; and based on the error tracking model of the controller and the adaptive gain and the adaptive law of the controller, designing an adaptive high-order sliding mode controller so as to carry out adaptive high-order sliding mode control on the high-altitude table air inlet environment simulation system. According to the invention, the adaptive high-order sliding mode controller is designed, and the response speed and the anti-interference capability of the high-altitude platform air inlet environment simulation system are improved by using the adaptive gain and the adaptive law designed by the integral terminal sliding mode function; and therefore, the air inlet pressure value can still be kept and the set pressure value can be accurately tracked under the condition that the air flow of the engine violently fluctuates due to the quick action of the throttle lever of the engine.
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Citation Information

Patent Citations

  • High-altitude table air inlet system anti-interference control method based on improved tracking differentiator

    CN117130267A

  • Intake pressure system identification method based on WOA-BP neural network

    CN117852392A