运载器

对运载器水下所受到的随机干扰进行了探讨。

The underwater random disturbances acting on the carrier are investigated .

运载器垂直出水弹道姿态角奇异性问题研究

On Singularity Problem of Water-exit Trajectory of the Missile Carrier

本文提出了适用于运载器数字姿控系统的P域与S域近似分析综合方法，给系统设计乃至考虑元件非线性以及应用实物实测频率特性带来了方便。

This report presents approximate analysis and synthesis methods of a digital attitude control system of an aerospace vehicle in the P-domain and S-domain .

重复使用运载器气动性能CFD研究

CFD Study of Aerodynamic Performance of Reusable Launch Vehicle

可重复使用运载器RCS修正脉冲调宽算法研究

Research on Revised Pulse Wide Modulation of Reaction Control System for Reusable Launch Vehicle

基于Vega的水下运载器视景仿真技术

A Visual Simulation Technique of the Underwater Vehicles Based on Vega

CCV水下运载器系统结构及其模糊自校正解耦控制

The Structure of CCV Subsea Vehicles and its Fuzzy Self-tunning Uncoupled Controller

通过对现场可编程门阵列（FPGA）的重构，星载计算机实现对运载器与卫星的控制与管理，并能够进行故障处理及在轨升级。

Through the fast dynamic reconfiguration of FPGA , the OBC could control the launch vehicle , and implement function switching , fault handling and upgrading when a small satellite is in orbit .

可重复使用运载器K-1的回收系统设计概况

Recovery system design of the k-1 reusable launch vehicle

利用捷联惯导（SINS）、GPS定位系统和多普勒计程仪（DVL）进行组合导航是水下运载器导航定位的有效方式。

It is an effective way in integrated navigation by using Strapdown Inertial Navigation System ( SINS ), GPS and Doppler Velocity Log ( DVL ) .

天地往返可重复使用运载器（RLV）在未来天战中将扮演重要角色。

Reusable Launch Vehichas ( RLV ) will play an important role in future outer space warfare .

应用CFD方法研究了两级重复使用运载器上升段和轨道器再入段的气动性能。

The aerodynamic performance of a tandem two-stage-to-orbit ( TSTO ) reusable launch vehicle ( RLV ) and its reentry orbiter are studied through employing computational fluid dynamic ( CFD ) method .

在大深度和危险区域，有缆遥控水下运载器（ROV）发挥了更大的优势。

In the deep and dangerous regions of the deep-sea , Remote Operated Vehicle ( ROV ) have been playing a crucial role .

紧接着，针对POGO振动的特性，将航天运载器分为两个系统：结构系统和推进系统，分别建立了两个系统的模型并进行了分析。

Considering the characteristics of POGO vibration , the space vehicle was divided into two systems : structure system and propulsion system .

研制轻质高强度的低温贮箱是美国发展重复使用运载器（RLV）的最关键技术之一。

To develop light weight and high strength tank for low temperature condition is one of the most key technologies of Reusable Launch Vehicle ( RLV ) .

基于古典控制理论和BTT倾斜转弯控制技术，设计了可重复使用运载器（RLV）的大气层内姿态稳定控制系统。

Focused on the problem of reusable launch vehicle ( RLV ) attitude control , an engineering attitude control system based on the classical control theory and BTT technology was designed .

就是对于这一个理由无人水下运载器（UUV）是将来的水雷-对抗应用最前线，而且他们为什么将会延伸主要存在滨海战斗空间。

It is for this reason that UUVs are coming to the forefront of mine-countermeasures practices , and why they will continue to be a major presence in the littoral battlespace .

水下无人运载器（UUV）往往由轴承、电机等大量旋转部件构成，其噪声主要是由机械振动引起。

Unmanned Undersea Vehicles ( UUV ) are often consist of a large number of rotating parts , such as bearings and motors . The noise of UUV is mainly caused by mechanical vibration .

基于非线性动态逆理论，设计了亚轨道可重复使用运载器（SRLV）的再入控制律。

The objective of this paper is to design the reentry flight control laws for the Suborbital Reusable Launch Vehicle ( SRLV ) based on nonlinear dynamic-inversion .

国际ARGO计划对我们的启示水下运载器是随着海洋资源开发和研究的不断深入以及国防的需要而产生和发展起来的高新技术，是海洋高科技的重要组成部分。

The Active Affect of Taking Part in the International ARGO Plan for Developing Ocean Technology in China Underwater vehicles , which are important in the architecture of ocean technology , belong to a new technology with the developing of national defense and exploitation of ocean resource gradually .

重复使用运载器末端能量管理段制导系统仿真

Terminal Area Energy Management Guidance Scheme Simulation for Reusable Launch Vehicle

可重复使用运载器制导控制方案初步分析

A Simple Analysis for Guidance and Control System of Reusable Launcher

美国重复使用运载器的发展历史、现状及启示

Development History , Current Status and Revelation of RLV in U.S.A

航天运载器支架式主结构承载性能的有限元分析

Load-bearing Capacity Analysis of Primary Truss Structures of Space Launch Vehicles

侧喷流直接力控制的运载器姿态稳定问题研究

Research on Attitude Stabilization Problem for Control System with Lateral Jet

重复运载器金属热防护系统的述评

Review of Metallic Thermal Protection System for the Reusable Launch Vehicle

运载器级间冷分离使用直接力姿控方法研究

Research on launch vehicle attitude control using direct force during stage-separation

用于大型运载器模态试验的油气支承系统

Oil-Air Support System Uesd to Modal Test for Large-Sized Launch Vehicle

可重复使用运载器磁悬浮助推发射参数研究

Study on Parameters of Magnetic Launch Assist for Reusable Launch Vehicles

可重复使用运载器复合材料低温贮箱应用研究

Study on application of composite cryogenic tank for reusable launch vehicle