thrust vector control

Unsteady characteristic research of startup process of secondary hot gas injection thrust vector control system

燃气二次喷射推力矢量控制系统启动过程非定常效应研究

Computational investigation of secondary flow thrust vector control technology used in a convergent-divergent nozzle ;

为了使导弹获得更高的机动性、敏捷性和导引精度，大多采用推力矢量控制方案。

Study on model reference robust control of thrust vector control system

推力矢量控制系统的参考模型鲁棒控制研究

Dynamic calculation on thrust vector control system for solid rocket motor

固体火箭发动机推力向量控制系统动力学计算

The program and calculation for thrust vector control system

推力向量控制方案及计算

The Application Analysis of Thrust Vector Control Systems of Air to Air Missile

推力矢量技术在空空导弹上的应用分析

Thrust vector control is an important technology for fighter .

推力矢量控制技术是当今世界战斗机技术研究的一个热点。

Analysis of Second Gas Injection Affecting Factor on SRM Thrust Vector Control

气体二次喷射SRM推力矢量控制影响因素分析

Thrust vector control for solid plug nozzle based on secondary injection

固体塞式喷管二次喷射推力矢量控制

Test Studies of Underwater Thrust Vector Control Performance

水下推力矢量特性试验研究

The Effect of Thrust Vector Control on the Performance of Turbofan Engine

矢量喷管控制对发动机性能的影响

Investigation on secondary gas injection for solid rocket motor based on thrust vector control

基于推力矢量控制的固体火箭发动机气体二次喷射研究

An Analysis on the Combination of Aero / Thrust Vector Control Surfaces

气动/推力矢量控制面融合方式研究

This method increase the damping ratio of the thrust vector control system and improve the system performance .

该方法提高了推力矢量电液位置伺服系统阻尼比，改善了系统的动态性能。

Thrust vector control technology and modern aircraft

推力矢量控制技术与现代飞机

Mathematical Model of Elasticity Missiles with Swing Nozzle Thrust Vector Control

采用摆动喷管推力矢量控制弹性弹体数学模型建立

Investigation of Thrust Vector Control by Differential Throttling

差分流量调节推力矢量控制研究

Research on the Attack Zone Simulation of a Kind of Air-to-air Missile with Thrust Vector Control

某型推力矢量控制空空导弹攻击区仿真研究

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

可延伸出口锥对推力向量控制系统稳定性的影响

Application of Redundancy Technigue in Servomechanism of Rocket Thrust Vector Control

冗余技术在火箭推力矢量控制伺服系统中的应用

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

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 Research on the Short Range Upper Armor Attack Trajectory by Using Both Atmospheric Force and Thrust Vector Control

气动力与推力矢量控制近距击顶弹道研究

Thrust Vector control is one of objects being seeked by engineers in rocket propulsion area .

流场控制以及基于此的发动机推力方向控制长期以来都是国内外火箭推进领域广大工程技术人员追寻的目标之一。

The thrust vector control ( TVC ) performance test of solid rocket motor is presented in this paper .

本文介绍了固体火箭发动机水下推力矢量特性试验。

And the research and development of motor energy management and thrust vector control ( TVC ) technique are being carried out .

发动机能量管理和向量控制技术的研制与开发工作正在开展之中。

Based on laser propulsion thrust vector control , a thrice reflecting focus system is put forward , designed and fabricated .

基于激光推进推力矢量控制，提出、设计并加工了一种三次反射激光聚焦系统。

The force for thrust vector control produced by the secondary injection gets bigger with the increase of flow mass and angle .

塞式喷管轴向力的增加随着二次流流量的增加而增加，但是二次流对轴向力的增加与二次流喷射的角度成反变关系。

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 .

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。

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 .

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。

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 .

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。