1)  Attitude-control thruster~+
姿控发动机+
2)  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。
3)  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。
4)  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
5)  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。
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。
参考词条
补充资料:姿态控制发动机
      见导弹推进系统。
  

说明:补充资料仅用于学习参考,请勿用于其它任何用途。