rlv
英
美
网络 可重复使用运载器; 可重复使用飞行器; 重复使用运载器; 可重复使用运载火箭; 火箭
双语例句
- Navigation Device Scheme and Information Processing Method of RLV
RLV导航系统硬件配置方案及信息处理技术 - Re-Entry Attitude Two-Loop SMC Control and Rudders-Nozzles Blending Selection Allocation of RLV
RLV再入姿态双环滑模控制及舵喷混合配置 - A new reentry guidance algorithm for RLV ( reusable launching vehicle) is presented.
提出了一种针对可重复使用运载器的再入制导算法。 - A survey of current RLV concepts in the U.S.
美国可复用运载器现行方案概况。 - To research the trajectory design method for terminal area energy management ( TAEM) of reusable launch vehicle ( RLV), the method basing on nonlinear equations of motion is designed.
为了研究重复使用运载器末端能量管理段的下滑轨迹线设计，给出了基于高度和动压的质点动力学的设计方法。 - This paper is major in the preliminary wing design for the Reusable Launch Vehicle ( RLV).
本文研究可重复使用运载器机翼外形的初步设计和优化方法。 - 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.
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。 - Reentry guidance law design for RLV based on predictor-corrector method
基于预测校正方法的RLV再入制导律设计 - A parallel one-dimensional model for transient thermal analysis of the metallic thermal protection system ( MTPS) for reusable launch vehicle ( RLV) is established.
建立了可重复使用运载器金属热防护系统瞬态热分析的并联一维模型。 - Parameterization Method and Constraints Transformation Method for RLV Reentry Trajectory Optimization Using Genetic Algorithm
飞行器轨迹优化应用遗传算法的参数化与约束处理方法研究 - Thermal Model Study of RLV Ceramic Thermal Protection System
RLV陶瓷热防护系统热分析模型研究 - Gravity acceleration module and atmosphere module, etc. are used to calculate environment parameters.
这些模块包括环境库中的重力加速度模块、大气模块等，他们用来计算RLV飞行过程中的环境参数； - 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.
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。 - Health Management for Thermal Protection System on RLV and Landing Gear Design for an UAV
RLV防热系统健康管理及某型无人机起落架设计 - This monitoring system is based on the analysis of foreign monitoring systems of RLV thermal protection system and the real-time health monitoring system of X-33. Hence, this system is reasonable.
该监测方案的提出，是在认真分析了国外航天飞机关于防热系统的监测方案以及X-33验证机的实时健康监控方案的基础上进行的，因此是具有可行性的。 - In this paper, flight trajectories were designed for a small-scale model of a reusable launch vehicle ( RLV) according to the dropping missions.
根据投放任务要求设计缩比可重复使用空间飞行器（RLV）投放轨迹，并建立飞行动力学基本分析框架。 - Genetic algorithm optimization of RLV reentry trajectory
基于遗传算法的RLV再入轨迹优化设计 - Net and remote diagnose based on web service have been finished. A RLV healthy remote and diagnose system is developed and achieve prospective aim.
net的网络化远程监测和基于网络服务（WEBService）的远程诊断部分程序设计，以航天器为对象，开发了RLV健康监控与远程诊断系统，达到了预期的设计目的。 - The module of the visual simulation has been confirmed according to RLV flight course and virtual prototype system.
根据RLV飞行过程与虚拟样机仿真系统需求，划分RLV视景仿真飞行任务模块； - The thesis aims at setting up the dynamic virtual prototype for contacting series two stages of RLV system and simulating flight at ascent stage.
本文主要针对我国串联两级重复使用跨大气层飞行器设计方案，建立其动力学虚拟样机，并使用该样机对串联两级RLV的上升段进行仿真计算。 - A novel integrated guidance/ control simulation model with high accuracy for reusable launch vehicle ( RLV) was proposed.
提出并建立了一种可重复使用航天器（RLV）再入飞行综合制导/控制仿真模型。 - Design and analysis on dropping trajectories of RLV configuration
某RLV飞行器投放轨迹的设计与分析 - In this paper, the scheme of RLV's health manages and the theories of health monitoring of one sysem of RLV are researched.
本文主要研究了可重复使用跨大气层飞行器（RLV）健康管理系统（HMS）总体框架及其关键系统之一&有效载荷释放和回收系统的健康监控原理。 - In this paper, adaptive inverse attitude control of RLV ( reusable launch vehicle) is studied. The mathematical model of the orbiter is built and adaptive inverse attitude controller is designed.
本文对可重复使用运载器的自适应逆姿态控制进行了研究，以航天飞机轨道器为模型，建立了自适应逆姿态控制的数学模型，设计了自适应逆姿态控制方案。 - This system is developed for a national 863 project, RLV ( Reusable Launch Vehicle) Healthy Monitor and Diagnose Technology Research.
net的网络化监测诊断系统的方案和实现方法，并围绕国家863项目&可重复使用跨大气层飞行器健康监测与故障诊断技术，以地面远程监测和诊断的实际应用为对象，对基于。 - The monitoring system of thermal protection system of RLV including both on-board monitoring diagnosis system, ground remote monitoring diagnosis system and ground manual maintenance system was proposed.
提出了在轨监控诊断系统、地面远程监控诊断系统及地面人工维护一体化的航天飞机防热系统监测方案。 - In this paper, the goal and characteristics for RLV GN& C are outlined, and the current technology efforts are reviewed, and the additional work needed for making this goal a reality is proposed.
指出了RLV的GN&C系统的要求、特点，总结了近年来该领域的研究成果，提出了下一步需研究的问题。 - Thermal protection system is one of the key technology of reusable launch vehicle ( RLV).
热防护系统是保证航天运载器安全、快捷、经济飞行的关键技术之一。 - For the new magnetic launch assist horizontal takeoff vehicle concept, according to a conceptual analysis method, the study was performed about effect of launch parameters on reusable launch vehicle ( RLV) performance.
针对磁悬浮助推水平起飞运载器这种新型发射概念，采用概念性分析方法，研究地面发射参数对可重复使用运载器性能的影响规律。