推力矢量控制由燃气喷口实现。
建立了带推力矢量的涡扇发动机数学模型。
A mathematical model of turbofan engine with thrust vector control was established.
对带推力矢量飞机的飞控设计问题进行了研究。
The design of the flight control system with the vectored thrust is discussed.
它采用嵌入式使用推力矢量发动机可变面积喷嘴。
It features embedded engines using variable area nozzles with thrust vectoring.
本文介绍了固体火箭发动机水下推力矢量特性试验。
The thrust vector control(TVC) performance test of solid rocket motor is presented in this paper.
根据静力平衡原理，推导了求解推力矢量的一般方程。
According to the static balance principle, the general equations for solving the describing parameters are derived and proved reliable.
具有超强的机动性，由于其推力矢量发动机的允许急转弯。
He said it has super maneuverability due to its thrust-vectored engines that allow for sharp turns.
即将到来的测试活动将验证系统的火箭马达和推力矢量控制。
The upcoming test campaign will validate the system's rocket motor and thrust vector control.
结果表明，推力矢量技术是未来战斗机必不可少的关键技术之一。
The research results show that thrust vectoring technology is one of absolutely necessarily key technologies for future aircraft.
研究了九分力推力矢量测量误差分析方法，并计算了推力矢量测量精度。
What's more, the precision of thrust vector measurement is also calculated, depending upon the error analysis of nine-component model.
研究的结论可以为推力矢量发动机及燃气舵的结构设计提供直接的参考。
Therefore, this research would provide a instructive reference straight for the structure design of thrust-vectoring motor and jet et vane.
结合工程实际，论述和分析了推力矢量发动机燃气舵气动特性的设计过程。
The aerodynamics design process of jet vane of the thrust-vector motor is discussed by combining the practical engineering.
矢量喷管是先进战斗机的特征，本文讨论了实现推力矢量存在的技术难点。
As thrust vectoring nozzle is the feature of advanced fighters, the difficulties in implementing thrust vectoring are summarized.
围绕组合喷管及其流量分配调节和推力矢量技术，本文开展了系统性研究。
Systematic researches on combined nozzle and its flow regulation, as well as thrust vector technologies are carried out in this dissertation.
在探讨推力矢量描述参数及计算的基础上，提出了一种推力矢量测量方案。
After introducing and calculating the describing parameters of the thrust vector, this article puts forward a measurement scheme.
采用六分力试验技术对某推力矢量发动机燃气舵的气动特性进行了试验研究。
Computational investigation of secondary flow thrust vector control technology used in a convergent-divergent nozzle;
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.
以F - 15战斗机为例，研究了失速及推力矢量对飞机瞬时转弯性能的影响。
Taking the flight parameters of F-15 fighter as analysis background, the affection of stall and thrust vector on instantaneous turning performance is studied.
文中针对推力矢量发动机燃气流场的流动问题，运用数值分析的方法进行了研究。
Using the numerical analyzing method, this article studied on the problem of the thrust-vectoring motor jet flow field.
首先，本文介绍了轨控发动机推力矢量测试原理，及静态标定装置设计方案的选择。
Firstly, measuring principle of the thrust measuring system is introduced, and how to select the design schemes of static calibration.
针对典型的推力矢量电液位置伺服系统提出参考模型模糊控制控制方法(MRFC)。
Model reference fuzzy control (MRFC) is introduced for a classical thrust vector electrohydraulic servo control system.
推力矢量控制技术和过失速机动使战斗机的空战效能大大增加，引起了世界各国的关注。
The thrust vectoring control technology and post-stall maneuverability enhance the aircraft's combat effectiveness greatly, and cause the worldwide interest.
建立了推力矢量测量九分力模型，提出了弧形轨的设计思想，解决了九分力模型方程求解问题。
The thrust vector measurement nine-component model is established, and the design idea of curve rail can benefit the nine-component model solving is proposed.
介绍了差分流量调节的计算方法和内喷管与塞锥推力矢量变化的分析过程，计算产生的俯仰力矩。
The computing method of differential throttling and the analytical process of thrust vector of inner nozzle and plug were introduced. The generated moments of pitch were given.
利用数值模拟的方法，通过对逆流方案中喷管气动性能的研究验证了逆流推力矢量方案的可行性。
The feasibility of counterflow scheme is validated by research on the internal aerodynamic characteristics of nozzle using numerical simulation.
推力矢量控制，往往所取得的节流个别推力器或注入气体通过喷嘴壁造成的变化在当地的压力分布。
Thrust vector control is often achieved by throttling individual thrusters or by injecting gas through the nozzle wall to cause a change in the local pressure distribution.
对摆喷管推力矢量方式，获得了推力、侧向力、推力矢量角随发动机喷管偏角以及水深的变化规律。
For the movable TVC, the thrust and lateral forces with respect to nozzle deflection angles and the depth of water were obtained.
常规线性飞控系统针对推力矢量飞机这样的多控制冗余、非线性MIMO系统，无法实现非线性控制。
Conventional linear flight control systems do not satisfy nonlinear control requirement of aircraft with thrust vector, which is a multiple control redundances and nonlinear MIMO system.
首次推导了基于质量控制和推力矢量控制的一类无尾无舵翼碟形飞行器的空间六自由度运动动力学方程。
The six degrees of freedom dynamic equation of a kind of mass-controlled and thrust vectoring-controlled saucer-like air vehicles without tailes, wings and rudders was derived for the first time.
仿真结果表明，该控制律能控制推力矢量飞机顺利完成过失速机动，对系统模型的不确定性具有较强的鲁棒性。
The results show that the control law can control vectored aircraft to accomplish post-stall maneuvers very well and it is very robust to model uncertainty.
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