推力矢量控制

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

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

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。

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

气体二次喷射SRM推力矢量控制影响因素分析

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

通过Lambert定理给出了VIC方案中需要速度的计算模型，并采用非线性的推力矢量控制（TVC）方法分析了增益速度的导引算法。

Calculation model of velocity in the VIC scheme was presented by means of the Lambert theorem , and guide algorithm of velocity gain was analyzed by using non-linear thrust vector control ( VIC ) method .

从飞机的六自由度运动方程出发，结合推力矢量控制系统，进行三种典型过失速机动（眼镜蛇，尾冲，Herbst机动）的数值仿真，主要研究了每一种机动的操纵规律；

Based on the six degree of freedom dynamic equations of an aircraft with thrust vectoring system , mathematical simulations of three typical post stall maneuvers ( Cobra , Tail slide and Herbst turn ) are presented .

具有推力矢量控制系统的导弹流体动力

Fluid Forces on a Missile with Control System of Vectorial Thrust

推力矢量控制系统的参考模型鲁棒控制研究

Study on model reference robust control of thrust vector control system

冗余技术在火箭推力矢量控制伺服系统中的应用

Application of Redundancy Technigue in Servomechanism of Rocket 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

Mathematical Model of Elasticity Missiles with Swing Nozzle Thrust Vector Control

固体塞式喷管二次喷射推力矢量控制

Thrust vector control for solid plug nozzle based on secondary injection

综合飞行/推力矢量控制系统设计与仿真

Design and Simulation of Integrated Flight / Vectored Thrust Control System

针对推力矢量控制飞行进行了仿真研究。

A simulation about vector thrust control flight was completed .

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。

Thrust vector control is an important technology for fighter .

扰流片式弹射火箭推力矢量控制技术研究

Study on a Thrust-vector Control Technique of the Ejection-rocket with the Spoiler

气动/推力矢量控制面融合方式研究

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

基于虚拟样机技术的轴对称推力矢量控制伺服机构设计

Design of servo mechanism based on virtual prototype technology

推力矢量控制与飞机过失速机动仿真研究

A Study on the Thrust Vectoring Control and Aircraft 's Post Stall Maneuver

推力矢量控制在掠飞击顶弹道中的方案分析与优化

Scheme Analysis and Optimization on TVC in the Hedgehopping Upper Armor Attack Trajectory

差分流量调节推力矢量控制研究

Investigation of Thrust Vector Control by Differential Throttling

基于推力矢量控制的固体火箭发动机气体二次喷射研究

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

推力矢量控制与推力矢量喷管

Thrust vectoring control and thrust vectored nozzle

推力矢量控制技术与现代飞机

Thrust vector control technology and modern aircraft

垂直发射快速转弯气动力/推力矢量控制研究最大发射光线的垂直角

Efficiently Controlling Fast Turn of Tactical Missile Vertical Launching Vertical angle of maximum candlepower emission

再评推力矢量控制技术的发展

Again Reviewing Thrust Vectoring Control Technology

某型推力矢量控制空空导弹攻击区仿真研究

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

推力矢量控制飞行的仿真研究

Simulation of Vector Thrust Control Flight

而推力矢量控制对于实现战斗机的过失速机动是必不可少的。

And the thrust vec to ring technologies is essential to achieve the ability of post-stall .

气动力与推力矢量控制近距击顶弹道研究

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

应用扩展的分支和连续算法对推力矢量控制飞机的飞行动力学特性进行了研究。

This paper presents the flight dynamical behavior of the thrust vectoring aircraft with extended bifurcation and continuation methods .

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。

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