弹箭与制导学报
彈箭與製導學報
탄전여제도학보
JOURNAL OF PROJECTILES, ROCKETS, MISSILES AND GUIDANCE
2010年
2期
7-9,14
,共4页
飞行/推进综合控制%自抗扰控制%冲压发动机%超声速%解耦
飛行/推進綜閤控製%自抗擾控製%遲壓髮動機%超聲速%解耦
비행/추진종합공제%자항우공제%충압발동궤%초성속%해우
integrated flight-propulsion control%active disturbance rejection control%ramjet%supersonic%decoupling
为解决飞行/推进综合控制的多变量耦合控制问题,提出了采用自抗扰控制技术的方法.分别对速度控制回路和高度控制回路进行自抗扰控制器设计,将回路间的耦合作为扰动进行估计并抑制.速度控制回路使用二阶线性扩张状态观测器.高度控制回路采用俯仰角和高度内外回路控制,分别使用三阶线性扩张状态观测器.采用带宽来确定状态观测器的参数.仿真结果表明设计的控制器消除了高度和速度通道之间的耦合,具有一定的抗噪声干扰能力.
為解決飛行/推進綜閤控製的多變量耦閤控製問題,提齣瞭採用自抗擾控製技術的方法.分彆對速度控製迴路和高度控製迴路進行自抗擾控製器設計,將迴路間的耦閤作為擾動進行估計併抑製.速度控製迴路使用二階線性擴張狀態觀測器.高度控製迴路採用俯仰角和高度內外迴路控製,分彆使用三階線性擴張狀態觀測器.採用帶寬來確定狀態觀測器的參數.倣真結果錶明設計的控製器消除瞭高度和速度通道之間的耦閤,具有一定的抗譟聲榦擾能力.
위해결비행/추진종합공제적다변량우합공제문제,제출료채용자항우공제기술적방법.분별대속도공제회로화고도공제회로진행자항우공제기설계,장회로간적우합작위우동진행고계병억제.속도공제회로사용이계선성확장상태관측기.고도공제회로채용부앙각화고도내외회로공제,분별사용삼계선성확장상태관측기.채용대관래학정상태관측기적삼수.방진결과표명설계적공제기소제료고도화속도통도지간적우합,구유일정적항조성간우능력.
An active disturbance rejection control (ADRC) scheme was proposed to solve the multivariable coupling control problem of integrated flight-propulsion control.The active disturbance rejection controllers were designed for velocity control loop and altitude control loop respectively.The interaction between flight control and propulsion control was estimated as disturbance and rejected.The second-order linear extended state observer (ESO) was used for velocity control loop.The altitude control loop was treated as internal-external loop control of pitch angle and altitude.Two third-order linear ESOs were proposed in altitude control loop.These ESOs' parameters were adjusted by bandwidth.The simulation results demonstrate that the controller designed eliminates channel coupling of altitude and velocity,and be capable of resisting noise disturbance.