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。