The attitude control thruster (ACT) is the control component of the flight vehicle.
姿态控制推力器(act)是飞行器控制系统的执行部件。
This paper content is the flight vehicle stabilization loop analysis and the design.
本论文的内容是飞行器稳定回路的分析与设计。
Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics;
北京航空航天大学飞行器设计与应用力学系；
In this paper, principle, design and test result of MMW wide beam antenna on flight vehicle is introduced.
本文介绍一种用于飞行器上的毫米波宽波束天线的原理、设计方法和实验结果。
Error analysis, modeling and compensation of MEMS gyroscope and its application in navigation of flight vehicle are researched in this paper.
本文主要研究了微机电陀螺的误差分析、建模和补偿，以及在飞行器导航中的应用。
Assuming that noise is unknown but bounded, set membership identification problem for flight vehicle aerodynamic parameters is studied in this paper.
在噪声未知但有界的情况下，本文研究了飞行器气动参数的集员辨识问题。
The results show that optimum design of solid propulsion in single discipline doesn't stand for multi-disciplinary optimum design for flight vehicle system.
结果表明，固体推进单学科的最优设计不等价于飞行器总体多学科的最优设计；
When aerodynamic numerical simulation for flight vehicle and its components is conducted, the aerodynamic shape is generally given in the manner of discrete data.
对飞行器及其部件进行气动力数值模拟时，气动外形常常是以离散数据形式给出。
With the improving of modern advanced flight vehicle, more and more attentions have been paid to the asymmetric flow involved over slender bodies at high incidence.
随着先进飞行器的性能提高，大攻角非对称流动问题越来越受到重视。
In flight vehicle preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of flight vehicle configuration designs.
在飞行器的初步设计中，快速而有经济地估计出飞行器结构设计中的各种气动特性是非常必要的。
Compared with traditional design optimization method, MDO method can gain the optimum design for flight vehicle as well as the optimum thrust-time curves of booster.
与传统设计优化方法相比，MDO方法一次设计优化就可得到满足飞行器总体设计指标的最优设计，得到内外弹道相匹配的助推器最优推力-时间曲线。
The methodologies of Multidisciplinary Design Optimization(MDO)have revolutionary impacts on design field of flight vehicle, and have become a new independent discipline.
论述分析模型参数化建模在飞机多学科优化设计中的重要意义，提出一种机翼气动与结构分析模型参数化建模方法。
In this paper the results of calculations of the coefficients of skin friction and heat transfer (Stanton number) on the surface of hypersonic flight vehicle are presented.
本文给出了高超声速飞行器表面摩阻和传热系数(斯坦顿数)的计算结果。
RBCC engine performance analysis model plays an important part in scheme selection and model design for Hypersonic Flight Vehicle, RBCC engine design and performance analysis.
RBCC发动机性能分析模型在高超声速飞行器方案选择、总体设计以及RBCC发动机设计与性能分析等方面具有极其重要的作用。
The utility model can be applied in the aviation, astronautics, life fields and other fields, and can provide sufficient electric energy for the flight vehicle and the daily life.
本发明可应用于航空、航天、生活等领域，为飞行器及日常生活等提供充足的电能。
The virtual world structure for controlling the motion of the flight vehicle model is presented, and hereby a virtual world including the flight vehicle model and the scene model is built up.
给出了飞行器级间分离仿真时用于控制飞行器模型运动的虚拟世界结构，并且据此建立了一个包括飞行器模型和场景模型的虚拟世界。
However I still hesitate, not knowing to board which photonic flight vehicle, perhaps I should be rushing to board that flying plane which is a unique fighter here, and has an alarming speed.
但我仍犹豫不定，不知道应登上哪一架光子飞行车，或许我应抢登那架在这里独一无二的飞翔型战斗机，它毕竟速度惊人。
When the distance between the mass center of liquid and the mass center of flight vehicle is large, the influences to rocket flight ballistics become serious, which even induce flight instability.
当充液质心与飞行器质心的距离较大时，对飞行器弹道的影响较严重，甚至导致飞行不稳定。
In pursuit of flight, I'm also keeping my eye on the Puffin, a "personal air vehicle" that became an Internet sensation when NASA unveiled it in 2010.
在追寻飞行之梦的路途中，我也在密切关注“海雀”，那是NASA在2010年公布的“个人空中飞行器”，在公布伊始就在网络上引发了热潮。
There are several factors that can influence sonic booms -- weight, size, and shape of the aircraft or vehicle, plus its altitude, attitude and flight path, and weather or atmospheric conditions.
有几个因素可以影响音爆——飞行器的重量，大小，形状以及其飞行高度，姿势和路线，还有天气或大气状况。
In June, Musk's company staged a successful inaugural flight of its Falcon 9 launch vehicle from the Cape Canaveral Air Force Station adjacent to the Kennedy complex.
6月，马斯科的公司进入肯尼迪综合中心附近的卡纳维拉尔角空军基地进行了它的猎鹰9号飞行器的首次发射。
The 1-x will climb about 40km (25 miles) into the sky during the powered phase of its flight, continuously measuring vehicle aerodynamics, controls and performance of the rocket's first stage.
战神一号X型将上升到约40公里(约25英里)的高空，在其动力飞行阶段，将不间断地对其运载空气动力学指标、火箭的第一阶段的控制和表现进行测量。
The United News of India (UNI) said the Geosynchronous Satellite Launch Vehicle (GSLV) veered from its intended flight-path and disintegrated seconds after lift-off.
印度联合新闻社(uni)称该同步卫星发射载具(GSLV)在发射升空数秒后偏离了其预定轨道并瓦解了。
The developing tools for hypersonic vehicle, i. e. ground test, computation and flight lest all have limitations for simulating hypersonic flight.
高超声速飞行器的设计工具，即地面试验、计算和飞行试验，在模拟高超声速飞行方面都有其局限性。
Design technology for integration of air vehicle fuselage, propulsion system and lifting control surfaces to optimize aerodynamic performance throughout the flight regime of an unmanned air vehicle.
为了优化无人驾驶航空飞行器在整个飞行过程中的空气动力特性而使机身、推进系统和升力控制面一体化的设计技术。
To get the data of the micro air vehicle (MAV) 's attitude in true flight, the data transmit and receive equipment is the key technology.
要实现在真实飞行情况下对微型飞行器姿态等数据的测量，数据的无线收发是其关键技术。
A new method of design hypersonic vehicle trajectory tracking system using fuzzy control is presented to overcome the disadvantage of flight trajectory distribution caused by separation disturbance.
针对高超声速飞行器飞行过程中因干扰造成的飞行轨迹散布问题，提出了采用飞行器飞行轨迹的模糊控制设计方法。
With widespread adopting of the Active Control Technique(ACT) and Control Configuration Vehicle(CCV)and Fly-by- wire system, position of Flight ControlSystem(FCS) become even more significant.
在航空航天飞行器设计中，随着主动控制技术、随控布局及电传操纵系统的普遍采用，飞行控制系统的地位变得更为重要。
The paper presents a design approach based on extremum seeking for minimum power demand of formation flight of Unmanned Aerial Vehicle.
采用极值搜索方法，解决无人机紧密编队飞行中僚机所需动力最小化的问题。
The paper presents a design approach based on extremum seeking for minimum power demand of formation flight of Unmanned Aerial Vehicle.
采用极值搜索方法，解决无人机紧密编队飞行中僚机所需动力最小化的问题。
应用推荐