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- The work module of rudder was discussed and studied by simulation in side jet and aerodynamic compound control manner, the effect on guidance accuracy by control cycle of attitude control engine and action cycle of control loop was simulated. 重点对采用燃气动力/气动力复合控制方式中舵系统的工作模式进行了探讨及仿真研究，对姿控发动机控制周期及控制回路工作周期对制导精度的影响进行了初步仿真研究。
- attitude control engine thrust chamber 姿控发动机推力室
- Second stage attitude control engine 二级姿控发动机
- Static Characteristic Analysis of Attitude Control Engine 姿控发动机静态特性分析
- DSMC SIMULATION OF PLUME BACKFLOW FROM BIPROPELLANT ATTITUDE CONTROL ENGINE 双组元姿控发动机反流特性的DSMC模拟
- DSMC simulation of nozzle flow of bipropellant attitude control engine DSMC法模拟双组元姿控发动机喷管流动
- Analysis of Pressurant Characteristics of a Regulated Pressure-Feed Attitude Control Engine 恒压式姿控发动机增压气体特性分析
- 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°。
- attitude control engine 姿态控制发动机
- Third, multi-duty direction pattern microminiaturized attitude control module. 三是多任务指向模式的微型化姿控模块。
- I majored in Systems and Control engineering. 我的专业是系统控制工程。
- The attitude control system of maneuver missile head is designed by applyi ng nonlinear decoupling control law. 然后采用非线性解耦控制理论设计了机动弹头的姿态控制系统。
- To enhance the robustness of interceptor attitude control system, a switch control method is presented to control the attitude of interceptor. 摘要为增强拦截器姿态控制系统的鲁棒性，提出了一种切换控制方法来控制拦截器的姿态。
- The Attitude Control System( ACS) software is responsible for maintaining the attitude of the spacecraft. 姿态控制系统（CS）件负责维护航空器的姿态。
- SHANGHAI OUDA ELECTRIC CONTROL ENGINEERING SYSTEM CO., LTD. 上海欧达电气控制工程系统有限公司。
- The aerocraft attitude control is divided into two parts: attitude stabilization and attitude track. 本文将飞行器姿态控制分为：姿态稳定和姿态跟踪两种情况加以研究。
- NANJING YONGHUI ELECTRIC POWER CONTROL ENGINEERING CO., LTD. 南京永惠电力控制工程有限公司。
- M. Noton, Modern Control Engineering, Pergamon Press, 1972. 日)绪方胜彦，现代控制工程，科学出版社，1981。
- The attitude control system (ACS) ensures the satellite to keep running normally. 摘要姿态控制系统是卫星得以持续正常工作的保证。
- An attitude control law for single axial direction control of an exoatmospheric interceptor is put forward. 针对单轴定向大气层外拦截器设计了一种姿态控制律。
