柔性运载火箭姿态控制,attitude control of flexible launch vehicle
1)attitude control of flexible launch vehicle柔性运载火箭姿态控制
英文短句/例句
1.Based on Second-order Sliding Mode一种基于二阶滑模的柔性运载火箭姿态控制
2.The Application of Fuzzy Control Theory in Attitude Control of Launch Vehicle;模糊控制在运载火箭姿态控制中的应用
3.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
4.TERMINAL SLIDING MODE CONTROL OF COORDINATED MOTION OF FREE-FLOATING FLEXIBLE SPACE MANIPULATOR漂浮基柔性空间机械臂姿态与关节协调运动的Terminal滑模控制
5.aerodynamic characteristics of launch vehicle运载火箭空气动力特性
6.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
7.On attitude simulation of guided rocket projectiles with complete integrated GPS/INS navigation systemGPS/INS全组合制导火箭弹姿态仿真研究
8.Fault Diagnosis Expert System of Launch Vehicle Control System运载火箭控制系统故障诊断专家系统研究
9.Active Track Control and Vibration Reduction in Two-Degree Flexible Spacecraft with Uncertainty via Shaped Reference Trace and Adaptive Control基于整形器的两轴柔性航天器自适应姿态控制
10.Engineering Attitude Control System Design of Reusable Launch Vehicle可重复使用运载器的工程化姿态控制系统设计
11.Research on Attitude Stabilization Problem for Control System with Lateral Jet侧喷流直接力控制的运载器姿态稳定问题研究
12.Research on Launch Vehicle Attitude Control Based on Direct Lateral Force基于侧喷流直接力技术的运载器姿态控制方法
13.Saturn launch vehicle“土星”号运载火箭
14.Changzheng launch vehicle“长征”号运载火箭
15.Geo-synchronous satellite launch vehicle地球同步卫星运载火箭(运载火箭)
16.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
17.The Long March II C carrier rocket was developed by the China Institute of Carrier Rocket Technology.长征二号C运载火箭由中国运载火箭研究院研制开发。
18.The Development of Robotic GTA Welding Quality Control System for Five Port Connector on the Launch Vehicle Propulsion System运载火箭动力系统五通连接器机器人GTAW质量控制系统
相关短句/例句
launch vehicle attitude control system火箭姿态控制
1.This paper introduces the working principle of servomechanism in thelaunch vehicle attitude control system and puts forward the possibility that hydraulic accumulator is directly used as the driver of the launch vehicle attitude servo control system, based on the working characteristics of servomechanism, and the problems to solve.本文介绍了火箭姿态控制伺服机构的工作原理,并根据伺服机构在火箭姿态控制系统中的工作特点,提出了用液压蓄能器直接作为火箭姿态控制系统伺服机构动力源的可能性以及需要解决的问题。
3)flexible satellite attitude control柔性卫星姿态控制
4)rocket attitude火箭弹姿态
5)flexible rocket柔性火箭
6)Launch vehicle运载火箭
1.Fault diagnosis technology of launch vehicle based on distributed expert system;基于分布式专家系统的运载火箭故障诊断技术
2.Modeling and Simulation of Navigation Calculating Subsystem of Launch Vehicle;运载火箭导航计算子系统建模与仿真
3.Onboard real-time compression of launch vehicle telemetry images;运载火箭飞行状态图像箭上实时压缩技术研究
延伸阅读
柔性1.柔顺之性。
