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超空泡航行器極點(diǎn)配置變結構控制方法研究
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1.北京機電工程研究所

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TP13

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Study on Pole Assignment Variable Structure Control Method for Supercavitation Vehicle
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    摘要:

    超空泡航行器在航行過(guò)程中,尾部會(huì )周期性拍打空泡壁而表現出強烈的“尾拍”現象,尾部空泡是由空化器經(jīng)歷的歷史位置形成,呈現強烈的時(shí)滯特性,動(dòng)力學(xué)建模和穩定控制是制約其發(fā)展的核心難題。針對泡體耦合問(wèn)題,建立了空泡/剛體相對幾何關(guān)系一體化實(shí)時(shí)解算的動(dòng)力學(xué)模型。針對后體非線(xiàn)性特性,采用分段線(xiàn)性化方法,在保留后體尾拍非線(xiàn)性特性的基礎上,建立了面向控制的簡(jiǎn)化模型。為了解決超空泡航行器非線(xiàn)性時(shí)滯控制問(wèn)題,針對彈體運動(dòng)極其敏感、操縱效率高等特點(diǎn),采用極點(diǎn)配置的方式將控制模型配置到理想狀態(tài)。針對尾拍過(guò)程非線(xiàn)性和不確定極大的特點(diǎn),建立了面向擾動(dòng)的變結構控制器,實(shí)現超空泡航行器擾動(dòng)運動(dòng)控制。采用極點(diǎn)配置變結構控制方法,分別設計了滾轉通道和俯仰通道控制律。利用泡體耦合動(dòng)力學(xué)模型進(jìn)行6DOF控制閉環(huán)軌跡仿真,穩定巡航過(guò)程中深度控制誤差小于0.1m,滾轉角控制誤差小于4°,表明該控制方法能夠對航行器滾轉角和深度實(shí)現穩定控制,控制效果較好,能夠滿(mǎn)足超空泡航行器航行要求。

    Abstract:

    During the sailing of supercavitation vehicle, the tail will periodically beat the cavitation wall and show a strong "tail-beating" phenomenon. The tail of cavitation is formed by the historical position experienced by the supercavitation vehicle and presents a strong time-delay characteristic. Dynamic modeling and stability control are the core problems restricting its development. Aiming at the cavitation-body coupling problem, the dynamic model of the integrated real time solution of the relative geometry relationship between the cavitation and rigid body is established. Aiming at the nonlinear characteristics, the piecewise linearization method is used to establish a simplified control oriented model while preserving the nonlinear characteristics of the rear body tail beat. In order to solve the nonlinear time-delay control problem of supercavitation vehicle, the control model is configured to the ideal state by pole assignment in view of the characteristics of extremely sensitive movement and high control efficiency. A perturbation-oriented variable structure controller (VSC) was established to control the disturbance motion of the supercavitation vehicle due to the nonlinear and uncertain process. The control law of roll channel and pitch channel is designed by pole assignment variable structure control method. The simulation of 6DOF control closed-loop trajectory using the cavitation-body coupled dynamics model shows that the depth control error is less than 0.1m and the roll Angle control error is less than 4° during the stable cruise. The proposed control method can achieve stable control of the roll Angle and depth of the vehicle. The control effect is good and can meet the navigation requirements of the supercavitation vehicle.

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湯柏濤,張建宏,高曄,魏先利.超空泡航行器極點(diǎn)配置變結構控制方法研究計算機測量與控制[J].,2023,31(9):157-165.

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歷史
  • 收稿日期:2022-11-07
  • 最后修改日期:2022-12-16
  • 錄用日期:2023-01-03
  • 在線(xiàn)發(fā)布日期: 2023-09-18
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