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本文详细介绍“直接侧力控制”的一般概念、“直接侧力控制”的各种模态及其解耦控制规律。以英国“PARIS”飞机为对象,借助数字与模拟计算机对“直接侧力控制”进行研究。研究及计算结果表明:飞机装有直接侧力发生器能产生定常偏航率为1.63度/秒,侧向加速度为0.45g,侧滑角为2.37°和侧滑速度为20.99英尺/秒的直接侧力,直接侧力控制是改善投射精度和飞行航跡控制的一个好方法。
This paper introduces in detail the general concept of “direct lateral force control”, various modes of “direct lateral force control” and its decoupling control law. In the United Kingdom “PARIS” aircraft as the object, using digital and analog computers on the “direct side force control” to conduct research. The results of the study and calculations show that the aircraft is equipped with a direct side force generator capable of generating a direct yaw rate of 1.63 degrees per second, a lateral acceleration of 0.45g, a side slip angle of 2.37 ° and a skid speed of 20.99 feet per second Side force, direct lateral force control is a good way to improve projection accuracy and flight path control.