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Launch Vehicle Flight Control System 运载火箭飞行控制系统
Launch Vehicle Flight Control 运载火箭飞行控制
Launch vehicle flight simulation 运载火箭飞行仿真
Strategy Research on Unmanned Aircraft Vehicle Flight Control System Software 无人机飞行控制系统软件测试策略的研究
The launch vehicle lifts the satellite into orbit. 太空火箭将人造卫星送入运行轨道。
During the early stage of reusable launch vehicle(RLV) re-entry flight,reaction control system(RCS) is a major attitude control device. 可重复使用航天器再入过程初期,反作用力控制系统是其姿态控制的主要手段,结合气动舵面可以减小飞行器对该系统的总冲需求,提高飞行器动态响应特性。
Research of White-box-testing Test Cases Design for Unmanned Aircraft Vehicle Flight Control System Software 无人机飞行控制系统软件白盒测试用例设计研究
Responsible for the launch vehicle BOM maintenance. 负责量产车型零件清单维护；
Subsystems of flight control system II. 飞行控制系统的分系统2。
China Lanzhou Flight Control Co. 兰州飞行控制有限责任公司。
Vehicle Flight Control System 飞行器飞行控制系统
In this paper, flight trajectories were designed for a small-scale model of a reusable launch vehicle (RLV) according to the dropping missions. 摘要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。
Located atop the S-IVB, which is the third stage of the Saturn V, is the guidance and control equipment for the launch vehicle. 安装在“土星V”第三级S-IVB顶部的是发射飞行器的导航和控制设备。
The next flight control keys around, the space bar shooting. 上下左右键控制飞行,空格键射击。
A robust attitude control method for the implementation of initial reentry for reusable launch vehicle (RLV) was proposed. 给出了一种可重复使用航天器(RLV)再入初期鲁棒姿态控制方法。
Key then used, the flight control around key direction. 然后用上键飞翔,左右键控制方向。
Flight dynamics and control, vehicle design, optimization and its nume rical method are employed to optimize the ascent trajectories and airbreathing propulsion system performance of two-stage-to-orbit (TSTO) launch vehicles with horizontal takeoff (HTO). 基于Sanger的气动外形、推进系统模型、质量模型等，采用飞行力学、最优控制理论及其数值计算等方法，研究了二级入轨水平起飞载机最小起飞质量的上升轨迹，得到了给定任务需求条件下吸气式组合发动机总体性能（推力、燃料消耗率随飞行轨迹的变化规律）要求。
Flight controllers could no longer hear Glenn. 飞行指挥员们再也无法听到格伦的声音。
The temperature regulation system optimizing control for multi-function launch vehicle of certain missile adopted 4 arms to control work current commutation. 某型导弹多功能发射车调温系统发射筒半导体致冷器的优化控制,使用4个桥臂控制工作电流换向。
FLIGHT CONTROLS HYDRAULIC SHUTOFF VALVES. 飞行操纵液压关断活门。