Application of Variable Structure Control in Missile Electromechanical Actuator System
Parameter variation and load disturbance will have great influence on the performance of missile electromechanical actuator system and further on the performance of the entire missile system during the missile flight process. To solve this problem, a variable structure control system for missile electromechanical actuator system was proposed in this paper. To verify the proposed control scheme, simulation has been performed for different system parameters. Simulation results indicate that the proposed variable structure control method can provide the properties of robustness to load and environment disturbance and insensibility to parameter variation. So it is very suitable for complicated and variable flight environment of missile.
Yuan Gao Liang-xian Gu Lei Pan
College of Astronautics Northwestern Polytechnical University Xian, Shannxi Province,710072, China College of Astronautics Northwestern Polytechnical University Xian, Shannxi Province, 710072, China
国际会议
长沙
英文
313-316
2008-10-20（万方平台首次上网日期，不代表论文的发表时间）