direct force flight control

基本解釋

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.
采用直接力控制可彌補常規(guī)飛機在軌跡操縱方面的不足，并產(chǎn)生某些新的運動模式。
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.
本文在深入研究現(xiàn)代控制方法（特征結(jié)構(gòu)配置方法），并將該方法應(yīng)用在常規(guī)飛機、推力矢量飛機和采用直接力控制飛機的飛行控制系統(tǒng)設(shè)計中。
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.
本文提出飛機中性穩(wěn)定技術(shù)應(yīng)用于綜合火力 /飛行控制系統(tǒng) ，給出了中性穩(wěn)定飛機結(jié)構(gòu)圖和動力學(xué)模型。