1)attitude control engine姿控发动机
1.Research on outlet pressure deviation calculation of pressure reducing valve for attitude control engine;姿控发动机减压阀出口压力偏差计算方法研究
2.The side jet technology of foreign advanced surface-to-air missiles is analyzed,disperse thrust models of 180 attitude control engines of patriot-III missile is built,and some optimized methods of ignite technology is studied,then the result of the simulation is presented.跟踪与分析国外先进防空导弹的姿控发动机控制技术,以美国PAC-3导弹为例,对姿控发动机组建立离散模型,然后采用一定的优化方法,对其点火方法作了研究,并提供仿真结果。
3.Using the plentiful software and USB interface of PC,taking FPGA as the core,controling the correspondence of the chip of USB,the automatic test of multi-pulse attitude control engine system status and the ignition of multi-pulse attitude control engines were carried out in this paper.利用PC丰富的软件和USB接口,以FPGA为核心,控制USB芯片的通信,实现了多脉冲姿控发动机系统状态的自动检测和多脉冲姿控发动机的点火。
英文短句/例句
1.Control Law Design of Lateral Attitude Jets for Spinning Missile弹体自旋条件下姿控发动机控制律设计
2.Output-prediction-based Optimization Design of Missile Attitude Control by Lateral Jets基于输出预测的姿控发动机控制律优化设计
3.Study on NDT technology used in the general assembly of attitude control engines无损检测技术在姿控发动机总装中的应用探析
4.Research of Quick Data Dealing Techniques for Test of pose-control Engine姿控发动机试验数据快速处理技术研究
5.Development of High Precision Time-Order Control System About the Test of Bi-Propellant Attitude-Controlled Engine双组元姿控发动机试验高精度时序控制系统研制
6.An Inventigation on Dynamic Thrust Measuring Technolgy for an Atittitude Control Liquid Propellant Rocket Engine in the Ground Firing Test;姿控发动机高空模拟试车动态推力测试技术研究
7.Research on parasitical monofier circuit influence on liquid orbit attitude control engine solenoid valve resistance test寄生振荡电路对液体轨姿控发动机电磁阀门阻值测试影响研究
8.Development of Pulsating Thrust Measuring System of Attitude-control Rocket Engine;姿控火箭发动机脉动推力测试系统的研制
9.attitude control propulsion motor姿态控制推进电动机
10.The Effect of Temperature on Thrust Testing System of Attitude Control Rocket Motor;姿控火箭发动机推力测试系统温度影响研究
11.Attitude control is obtained by gimballing the engine up to ±7 degrees.姿态控制是由发动机摆动而得到的，摆动度最大为±7°。
12.Measurement Principle and Dynamic Performance of Pulse Thrust Vector Measuring System for Attitude/Orbit Rocket轨/姿控火箭发动机推力矢量动态测试系统测量原理与动态性能
13.The Chaotic Attitude Control in the Large Angle Attitude Maneuver of Liquid-Filled Flexible Spacecraft柔性充液航天器姿态转换机动及混沌姿态控制
14.Active Vibration Control of Flexible Spacecraft during Attitude Maneuver挠性航天器姿态机动的主动振动控制
15.LARGE ANGLE ATTITUDE MANEUVERS AND CONTROLS OF GYROSTAT SPACECRAFT陀螺体飞行器大角度姿态机动与控制
16.QUASI-EULER-ANGLES FEEDBACK CONTROL OF SPACECRAFT ATTITUDE MANEUVER航天器姿态机动的拟欧拉角反馈控制
17.Research on the Control Method of Parawing Posture of the Kite Generator;风筝发电机翼伞姿态控制方法的研究
18.Dynamic pelvis position control mechanism for a walking aided training robot助行训练机器人骨盆位姿控制机构动力学研究
相关短句/例句
attitude control motor姿控发动机
1.First a model of combined fire of motors for attitude control is developed,and then on the basis of this model,a firing rule of attitude control motor is designed and an analysis on the energy consumption efficiency is made under the condition of di-fferent position distribution of attitude control motors,finally the simulation result proves the fea.针对具有侧向脉冲推力和气动力复合控制的动能拦截弹,需要解决姿控发动机的组合点火问题。
2.The status and tendency of attitude control motors for satellites is briefly described.简要介绍了目前卫星姿控发动机的应用现状及发展趋势 ,提出了一种以光化学分解为基础的工作过程可控的固体姿控发动机新概念。
3)attitude control thruster姿控发动机
1.Experimental study on plume impingement effects of satellite attitude control thruster nozzle;卫星姿控发动机喷管羽流撞击效应试验
4)side jet姿控发动机
1.In missiles using direct force control systems, a high precision robust guidance law with low side jet consuming is required.最后进行了三维弹道仿真,结果表明:所设计的导引律攻击精度明显优于比例导引律,尤其是在目标机动较大情况下,保证了脱靶量在米级以内;所设计的导引律在制导初期对误差进行修正,因而末端弹道更为平直,同情况下所消耗的姿控发动机数目更少。
2.In this paper, an attitude control method using side jets of a kind of long-distance air defense missile is studied.以某型远程地空导弹为背景,研究了以姿控发动机作为执行机构下导弹的姿态控制问题。
5)attitude-control and orbit-control engines姿控轨控发动机
6)impulse attitude control motor脉冲姿控发动机
1.Endoatmospheric interceptor fast response control using impulse attitude control motor;大气层内拦截弹脉冲姿控发动机快响应控制
2.Four factors are used to describe the influence of jet interaction for the missile using impulse attitude control motors in the equations of motion.姿控发动机的点火指令按等周期计算,通过分析导弹在一个点火周期内的动力学,用李雅普诺夫函数设计指令趋近律,最后得到了离散化的舵指令和脉冲姿控发动机点火指令。
延伸阅读
姿态控制发动机 见导弹推进系统。
