摘要
与传统飞机使用的被动侧杆相比,主动侧杆系统提高了飞行员的飞行状态感知能力,帮助飞行员快速应对突发事件。本文针对主动侧杆非线性系统的建模与控制问题,为主动侧杆的关键部件及主要存在的非线性因素建立了数学模型。然后设计了主动侧杆系统的控制方案,其中包括力感曲线模型与基于模糊鲁棒控制的位置伺服控制方法,以补偿系统受到的非线性因素影响。仿真结果表明,所设计的系统能够很好地控制侧杆位移和力反馈,并抑制机械非线性对于系统的干扰,验证了控制方法的有效性。本文所提出的建模与控制方法对于主动侧杆系统的未来研究具有一定的参考价值。
Compared with the passive sidestick used by traditional aircraft,the active sidestick system improves the pilot's flight state perception ability and helps the pilot to quickly respond to emergencies.Aiming at the modeling and control of the nonlinear system of the active sidestick,this paper establishes a mathematical model for the key components of the active sidestick and the main nonlinear factors.Then the control scheme of the active sidestick system is designed,including the force sense curve model and the position servo control method based on fuzzy robust control to compensate for the influence of nonlinear factors on the system.The final simulation results show that the designed system can control the displacement and force feedback of the sidestick well,and suppress the interference of mechanical nonlinearity to the system,which verifies the effectiveness of the designed control method.
作者
王灿
杨忠
陈旭
杨乐
杨凯
张诚
WANG Can;YANG Zhong;CHEN Xu;YANG Le;YANG Kai;ZHANG Cheng(College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;China Aviation Industry Jincheng Nanjing Electrical And Engineering Research Center,Nanjing 210016,China)
出处
《应用科技》
CAS
2023年第5期157-162,共6页
Applied Science and Technology
基金
中国航空工业集团公司金城南京机电液压工程研究中心科技项目.
关键词
主动侧杆
触觉提示
电机矢量控制
非线性控制
力反馈
铰链力矩
摩擦补偿
间隙补偿
Active sidestick
Tactile cue
Field Oriented Control
Nonlinear control
Force feedback
Hinge moment
Friction compensation
Backlash compensation
