根据飞机给出的纵向简化模型，设计飞机纵向增稳系统-According to the vertical plane gives the simplified model, the design aircraft longitudinal stability augmentation system

基于压电双晶片的微型无人机增稳驱动系统研究Based on piezoelectric bimorph micro UAV stability augmentation system for driving-Based on piezoelectric bimorph micro UAV stability augmentation system for driving

关于直升机增稳控制系统设计中高度以及位置x，y的matlab仿真程序，利用optimization得到最优参数，效果很好，满足快速性稳定性的要求-Helicopter stability augmentation control system design, height and location x, y matlab simulation program, the use of optimization to get the optimal parameters, the effect is