direct thrust force control

基本解釋

Direct thrust force control method for the linear motor in theory and experiment has been further studied.
對(duì)適合直線電機(jī)直接推力控制的方法進(jìn)行理論分析和實(shí)驗(yàn)研究。
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(jī)、推力矢量飛機(jī)和采用直接力控制飛機(jī)的飛行控制系統(tǒng)設(shè)計(jì)中。