turning thrust vector

用法例句

Investigation on a thrust vector design scheme of ramjet;

一种冲压发动机推力矢量设计方案研究

Design of thrust vector measuring system for engine;

发动机推力矢量测试系统的设计

Researches of dorsal support interference in low speed wind tunnel thrust vector test;

低速风洞推力矢量试验背撑干扰特性试验研究

Attitude control of thrust vectoring unmanned aerial vehicle based on brain emotional learning

基于大脑情感学习的推力矢量无人机姿态控制

A study on the integrated flight and propulsion control system(IFPCS) with the thrust vectoring for a cer-tain type of unmanned aerial vehicle(UAV) is carried out.

以某无人机为背景,主要研究大机动时带推力矢量的综合飞行/推进控制系统的设计方法。

The design of the flight control system with the thrust vectoring is discussed.

研究了带推力矢量飞机过失速非线性飞行控制问题。

In this paper,six degrees of freedom model of air-to-air missile is established by using bank to turn(BTT) and the thrust vector control(TVC) technologies.

应用倾斜转弯(Bank to Turn,BTT)及推力矢量控(ThrustVector Control,TVC)技术设计并建立了空空导弹六自由度模型。

Three-kind thrust vector control (TVC)rudder systems are briefly introduced.

简要介绍了三类推力矢量舵系统，分析了几种主要推力矢量舵系统的操作效率。

The aerodynamics design process of jet vane of the thrust-vector motor is discussed by combining the practical engineering.

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 aerodynamic properties of thrust-vectoring et vane are studied by six-component forces test and all the forces on the vane flake and the force moments around the vane flake axes are obtainted.

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。

This paper considers UCAV with vector thrust(UCAVVT)as research object,builds a flight dynamic model of UCAVVT and a flight control model of missile guide as research base.

无人战斗机逃逸概率是无人机设计的重要指标之一,提高无人机飞行时的可用过载能够提高其逃逸概率,另外无人机的机动也对其逃逸概率有重要影响,如何评判在各种机动情况下无人机对导弹的平均逃逸概率与其过载的关系是无人机设计师和军方十分关注的问题;论文以带矢量推力无人战斗机(UCAVVT)作为研究对象,建立其飞行动力学及导弹导引飞行控制数学模型,通过预先假定无人机做典型机动的概率,由计算机仿真导弹与无人机的相对飞行轨迹,研究讨论在各种机动下UCAVVT在导弹攻击下的平均逃逸概率,并对计算结果进行了分析,得出了一些重要结论,对带矢量推力无人战斗机的总体设计具有一定的参考价值。

Research and Development of the Thrust Vector Measuring System for Rocket Motor;

火箭发动机推力矢量测试系统的研制

A study for thrust vector control of aerospike nozzle based on second injection

塞式喷管二次喷射推力矢量控制研究

Singularity analysis of axisymmetric vectoring exhaust nozzle

轴对称推力矢量喷管运动奇异性分析

Development on Thrust Vector Measuring Platform for Rocket Motor Thrust Vector Measuring System;

火箭发动机推力矢量测试系统测力平台的研制

Efficiently Controlling Fast Turn of Tactical Missile Vertical Launching

垂直发射快速转弯气动力/推力矢量控制研究

A simulation about vector thrust control flight was completed.

针对推力矢量控制飞行进行了仿真研究。

Research on Nonlinear Flight Control Law Design of Aircraft with Vectoring Thrust;

推力矢量飞机非线性飞行控制律设计研究

Research on the Thrust Vector Measuring System for Rocket Motor Dynamic Characteristics;

火箭发动机推力矢量测试平台动态特性的研究

Research and Development of Calibration Devices for Rocket Motor Thrust Vector Measuring System;

火箭发动机推力矢量测试系统标定装置的研制

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

扰流片式弹射火箭推力矢量控制技术研究

Development of Dynamic Calibration Setup for Engine Thrust Vector Measurement System;

发动机推力矢量测试系统动态标定装置的研制

Post Stall Dynamic Boundaries and Agility Research for Thrust Vector Controlled Aircraft;

推力矢量飞机过失速动态边界和敏捷性研究

Attitude control of thrust vectoring unmanned aerial vehicle based on brain emotional learning

基于大脑情感学习的推力矢量无人机姿态控制

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

Research on the control over underwater high-speed projectiles based on thrust vector

基于推力矢量的水下高速射弹控制研究

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

Unsteady internal performance study of counterflow vectoring thrust nozzle

逆流推力矢量喷管的非定常内流性能研究

Research on the Theory & Method of Trust Vector Measurement and the Automatic Test Technology in Rocket Engine Ground Test;

火箭发动机推力矢量测量理论、方法与自动测试技术研究