推力向量控制

固体火箭发动机推力向量控制系统动力学计算

Dynamic calculation on thrust vector control system for solid rocket motor

推力向量控制方案及计算

The program and calculation for thrust vector control system

气体二次喷射推力向量控制数值仿真

Numerical simulation of secondary gas injecting for thrust-vector-control

可延伸出口锥对推力向量控制系统稳定性的影响

The Effects of the Extendible Exit Cone on Stability of the Thrust Vector Control System

对大型运载火箭的固体助推器，通常采用摆动喷管推力向量控制。

The deflecting nozzle thrust vector control is usually used in a large solid booster .

在不增加激励器输入功率的情况下，带倾角激励器可以极大地增加主流偏转角度，推力向量控制效果很好。

The actuator at an angle can change greatly the primary jet direction and has a good effect on thrust vectoring without increasing input power .

本文归纳推力向量控制的主要方案，着重介绍摆动喷管、流体二次喷射方案的计算思路和结果。

The authors summary the programs for thrust vector control systems and emphatically introduce the calculating idea and results for movable nozzles and fluid secondary injection .

为使飞行器能在主动段很快地进入到理想弹道上，系统采用了非线性的推力向量控制及预测制导方法。

In order to enter into the ideal trajectory with minimal energy , the nonlinear thrust vector control and the prediction guidance are adopted in the missile guidance control system .

喷管是固体火箭发动机推力向量控制系统的重要组成部分，高效能的喷管设计对发动机的性能至关重要。

Nozzle is an important part of the thrust vector control system of solid rocket motor and high-performance design of a nozzle plays an important role in the performance of the motor .

介绍了喷管可延伸出口锥对大型固体火箭发动机推力向量控制系统稳定性的影响，并提出了改善其系统稳定性的措施。

The effects of the extendible exit cone on stability of the thrust vector control system of largescale solid rocket motor are presented and the measures for improving the system stability are suggested .