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研究采用“直接升力控制系统” ,在俯仰角保持不变 ( =const)的情况下 ,空中加油时飞机的飞行动力学和飞行控制问题。采用F - 15飞机 (静不安定飞机 )参数 ,完成了飞机空中加油过程线化模型的建立和运动关系的推导 ;进行了空中加油闭环过程的计算机模拟 ;结果证明这种方法是有效的。
The study used a “direct lift control system” to study aircraft flight dynamics and flight control problems with refueling at pitch angles ( = const). Based on the parameters of the F - 15 aircraft (static instability aircraft), the establishment of the linearization model and the kinematic relation of the air refueling process were completed. The computer simulation of the air refueling closed - loop process was carried out. The results show that this method is effective.