The adaptive optimal decoupling control method of helicopter rotor concordant loading system was discussed.
研究了直升机旋翼协调加载系统的自适应最优解耦控制问题。
2
Based on the dynamics analysis of the screw rotor, the "by step check" interference detection program is developed and the movement interference under the state of loading is detected.
在螺杆转子动力学分析的基础上，编写了“单步检测”程序，检查了负载状态下的运动干涉情况。
3
On the other hand, the shock wave position of tip region moves backwards, the loading distributions of tip region have been changed, which lead to the increase of rotor operation range.