direct force flight control

基本解释

The disadvantages of normal aircraft in flight path control can be overcome by using direct force control, and some new motion modes can be realized.
采用直接力控制可弥补常规飞机在轨迹操纵方面的不足，并产生某些新的运动模式。
Flight control systems are designed by eigenstructure assignment method for traditional aircraft, aircraft with thrust vector and aircraft with direct force control in this paper.
本文在深入研究现代控制方法（特征结构配置方法），并将该方法应用在常规飞机、推力矢量飞机和采用直接力控制飞机的飞行控制系统设计中。
In this paper, the authors try to apply neutral stability mode of the aircraft direct force Control technology to the air-to-air gunnery mode of the integrated flight/fire control system.
本文提出飞机中性稳定技术应用于综合火力 /飞行控制系统，给出了中性稳定飞机结构图和动力学模型。