【摘要】 基于直升机非线性动力学方程 ,在简化悬停和低速飞行模态的推力扭矩模型的基础之上 ,用多变量线性鲁棒控制、遗传模糊控制和非线性跟踪控制等 3种不同方法 ,设计了飞行控制系统 ,并通过各种飞行仿真验证了飞行控制性能 ,分析与比较了这 3种方法的特点更多还原

【Abstract】 The design of a flight control system for an autonomous helicopter is performed, based on nonlinear dynamic equations and a simplified thrust-torque generation model in the hovering and low speed flight regimes and using three design techniques: linear robust multi-variable control, genetic fuzzy control and nonlinear tracking control. The controller performances derived from the three design techniques are evaluated in various simulated maneuvers.更多还原