摘要
文章推导了具有双执行机构的十字梁实验系统三自由度运动动力学方程，设计了一个基于趋近律的滑模变结构控制器，对纵向运动模型进行了数学仿真，为深入探讨气动-质量矩复合控制奠定了基础。
The three degrees of freedom dynamic equation of gas-flotage crossbeam with double operators based on composite control of aerodynamics-mass moment was derived. A sliding mode variable structure controller based on reaching law was designed in this paper. Simulation and practicality experiment about the crossbeam attitude confined to vertical plane was performed, which laid a foundation on developing the composite control of aerodynamics-mass moment control.
出处
《海军航空工程学院学报》
2008年第4期371-374,379,共5页
Journal of Naval Aeronautical and Astronautical University
关键词
复合控制
共栖
十字梁
趋近律
composite control
commensalisms phenomenon
crossbeam
reaching law
