As a result of applying this method, simple and optimal control laws have successfully been developed for the active suppression of wing bending-torsion flutter and under-ballanced aileron flutter using a single trailing-edge active control tab.

• 运用这种方法获得用单独后缘主控调整片抑颤的优化控制律,实现了对质量不平衡舵面颤振和翼面弯扭颤振的有效抑制。