兵工自动化
兵工自動化
병공자동화
Ordnance Industry Automation
2015年
10期
59-63
,共5页
自抗扰控制器%磁悬浮转子%解耦控制%扰动抑制
自抗擾控製器%磁懸浮轉子%解耦控製%擾動抑製
자항우공제기%자현부전자%해우공제%우동억제
ADRC%magnetically suspended rotor system%decoupling control%disturbance rejection
为了克服外部扰动影响磁悬浮转子悬浮稳定度和磁悬浮控制力矩陀螺输出力矩精度的问题,提出一种基于自抗扰控制器的磁悬浮转子扰动抑制方法.根据牛顿第二定律和陀螺技术方程建立磁轴承坐标系下磁悬浮转子系统的动力学方程,基于自抗扰解耦控制原理得到径向四通道解耦模型,设计各通道自抗扰控制器,从而实现转子系统径向四通道解耦和扰动抑制.与分散 PID加交叉反馈控制方法进行仿真对比,结果表明:自抗扰控制器具有良好的扰动抑制功能,能提高转子的稳定精度和控制力矩陀螺的输出力矩精度;因此,此方法不仅改善了解耦控制精度,而且提高了系统对外部扰动和参数变化的鲁棒性,可应用于磁悬浮控制力矩陀螺的高精度强鲁棒控制.
為瞭剋服外部擾動影響磁懸浮轉子懸浮穩定度和磁懸浮控製力矩陀螺輸齣力矩精度的問題,提齣一種基于自抗擾控製器的磁懸浮轉子擾動抑製方法.根據牛頓第二定律和陀螺技術方程建立磁軸承坐標繫下磁懸浮轉子繫統的動力學方程,基于自抗擾解耦控製原理得到徑嚮四通道解耦模型,設計各通道自抗擾控製器,從而實現轉子繫統徑嚮四通道解耦和擾動抑製.與分散 PID加交扠反饋控製方法進行倣真對比,結果錶明:自抗擾控製器具有良好的擾動抑製功能,能提高轉子的穩定精度和控製力矩陀螺的輸齣力矩精度;因此,此方法不僅改善瞭解耦控製精度,而且提高瞭繫統對外部擾動和參數變化的魯棒性,可應用于磁懸浮控製力矩陀螺的高精度彊魯棒控製.
위료극복외부우동영향자현부전자현부은정도화자현부공제력구타라수출력구정도적문제,제출일충기우자항우공제기적자현부전자우동억제방법.근거우돈제이정률화타라기술방정건립자축승좌표계하자현부전자계통적동역학방정,기우자항우해우공제원리득도경향사통도해우모형,설계각통도자항우공제기,종이실현전자계통경향사통도해우화우동억제.여분산 PID가교차반궤공제방법진행방진대비,결과표명:자항우공제기구유량호적우동억제공능,능제고전자적은정정도화공제력구타라적수출력구정도;인차,차방법불부개선료해우공제정도,이차제고료계통대외부우동화삼수변화적로봉성,가응용우자현부공제력구타라적고정도강로봉공제.
In order to overcome disturbance effect in stability of magnetic suspended rotor and output torque accuracy of magnetically suspended control moment gyroscope, this paper presents a disturbance rejection method of magnetic suspended rotor based on active disturbance rejection controller. The dynamics model of magnetic suspended rotor is established, decoupling model of radial four channel is obtained based on principle of ADRC, rotor radial four channel decoupling and disturbance rejection is achieved through ADRC. Through simulation, we find ADRC controller has good function of disturbance rejection, canimprove stability precision of rotor and output torque accuracy of control moment gyroscope. Therefore, this method not only improves accuracy of decoupling control, but also improves the robustness of system to external disturbances and parameter variations, and can be used in high precision strong robust control for magnetically suspended control moment gyroscope.