建立了运载器起飞段侧喷流直接力姿态控制模型。
A launch vehicle with lateral jet as its attitude control mechanism during ascending stage was proposed.
底喷流动具有添质加能和引射两种相反作用，并能消弱侧喷流对弹丸底部流动的影响。
The base bleed has two contrary action of providing energy and ejection, and it can weaken the effect of lateral jet upon base flow.
针对控制系统采用侧喷流发动机和栅格舵的新型小型多级固体运载火箭开展六自由度弹道仿真研究。
This article studies the six-degree-of-freedom trajectory simulation of small multiple stage solid launch vehicles with control systems using lateral jet thrusters and grid fins.
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