跟踪控制状态飞行员建模研究

Study of Modeling Pilot Pursuit Control Behavior

在跟踪飞行状态时,飞行员是按被跟踪状态量的速率信息和跟踪误差信息以一定的控制规律进行操纵的。研究了飞行员在跟踪控制状态时操纵模型的建立方法,即如何建立飞行员的控制规律。以光学助降人工着舰时飞行员下滑"m eatball"对中跟踪操纵为例,采用海军惯用的"backside"技术设计了飞行员控制规律的操纵增益参数,并辅以仿真验证。结果表明,跟踪控制状态飞行员建模的简化方法具有普遍意义。

In pursuit tracking flight, the output-rate and output error are combined by a pilot in a certain way to control the plane. An approach for modeling the pilot pursuit control behavior was studied, namely how to establish a pilot＇ s control law. Then, an application to the roger meatball correction, using backside techniques, with the optical landing aid system in carrier landing was presented. In the example, the key parameters in the pilot＇ s control law, pilot＇ s control gains, were designed. The result of the simulation reveals that the simplified approach for modeling the pilot pursuit control behavior has an universal significance.