论文部分内容阅读
对纵列式双旋翼直升机控制律构型进行了研究,并采用Dspace动态实时仿真系统对飞行控制律进行设计与仿真。其中包括Simulink/Control Desk交互、Dspace试验原理和步骤以及应用图形界面对仿真结果进行分析和评定。
The configuration of the control law of the tandem helicopter was studied and the flight control law was designed and simulated by Dspace dynamic real-time simulation system. Including Simulink / Control Desk interaction, Dspace test principles and procedures and the application of graphical interface analysis and evaluation of simulation results.