Research on Nonlinear Control of Digital Actuator Based on Electromechanical Co-Simulation
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Research on Nonlinear Control of Digital Actuator Based on Electromechanical Co-Simulation
基于机电联合仿真的数字化舵机非线性控制研究
Vol. 34, Issue 4, Pages: 419-423(2013)
作者机构:
中国空空导弹研究院
作者简介:
基金信息:
DOI:
CLC:
Published:2013
稿件说明:
移动端阅览
杨君君. Research on Nonlinear Control of Digital Actuator Based on Electromechanical Co-Simulation[J]. 2013, 34(4): 419-423.
DOI:
杨君君. Research on Nonlinear Control of Digital Actuator Based on Electromechanical Co-Simulation[J]. 2013, 34(4): 419-423.DOI:
Research on Nonlinear Control of Digital Actuator Based on Electromechanical Co-Simulation
摘要
为了分析非线性因素对空空导弹数字化舵机的影响
利用UG-ADAMS-ANSYS-MATLAB软件
建立了舵机的机电联合仿真模型
并将非线性因素细化到电动舵机的数学仿真模型中.在集成仿真环境下
对传动机构的摩擦、间隙、刚度等非线性参数进行了仿真.结合仿真分析结果
有效地解决了舵机控制的非线性因素问题.
Abstract
To analyze the influence of nonlinear factors on digital electromechanical actuator of an air-to-air missile
the mechanical and electrical co-simulation model was built by UG-ADAMS-ANSYS-MATLAB.The nonlinear factors were also refined to the mathematical model of the electric actuator.In the integrated simulation environment
simulation of nonlinear parameters
such as driving mechanism friction
the clearance and stiffness
was done.Comparing with simulation results
the nonlinear problems of electromechanical actuator are well resolved.
关键词
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references
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