Research on the Controlling Methods for Rudder Simulator Based on PXI

摘要：

Missile rudders are executive bodies of missile flight control system.All kinds of attitude motion of missile are depended on the actuator driver fins of rudder.The soft ware designs of the electrical servo system are completed after the hard ware designs are presented in details.Then simulation and analyses of the servo system are carried out.

作者: Xianjun Shi Huibo Lin Jian Liao

会议类型: 国际会议

会议名称: Asia Simulation Conference 2008/the 7th International Conference on System Simulation and Scientific Computing(2008亚洲仿真会议/第七届系统仿真和科学计算国际会议)(ICSC2008)

会议地点: 北京

会议语种:英文

在线出版日期: 2008-10-10（万方平台首次上网日期，不代表论文的发表时间）