The unmanned air vehicles tactical control system ( uav - tcs , for short tcs ) is aninnovation of the usage of uav . it aims to explore a common unit , which can control andcommand all uav from now to future 无人机战术控制系统(简称战术控制系统)是一种无人机使用概念创新,目标是研制出一个通用无人机控制单元,能够控制和使用当前和将来的各种无人机。
In the system construction analysis , the progress of the ucav is summarized and the ucavs is set up referring to the american examined ucavs and the construction of the unmanned air vehicle 在无人战斗机系统分析中，首先综述了无人战斗机系统研究进展，然后以无人机系统构成为基础，参考美国现有无人战斗机验证机系统和导弹系统建立无人战斗机系统并选定其子系统。
Compared with general aircrafts and ships , the wing - in - ground air vehicle features high aerodynamic efficiency , safety , high speed , comprehensive use and potential development toward huge vehicle of thousands tons 地效飞行器与一般的飞机和船舶相比,具有气动效率高、安全性好、速度快、可用作多方面的执行任务的交通工具,能向几千吨位的大型化发展等优势特点。
Flapping - wing micro air vehicles ( fmav ) are new conceptual air vehicles . they surpass the research fields of traditional airplane design and aerodynamics in relation to application technologies , and initiate the applications of mems technologies to aviation fields 微扑翼飞行器是一种模仿鸟类或昆虫飞行的新概念飞行器,在应用技术上它超出了传统的飞机设计和气动力的研究范畴,同时开创了微机电系统技术( mems )在航空领域的应用。
The paper mainly does research on simulation of the air - to - surface ( as ) attack mission . on the basis of that , as attack representative maneuver chains are designed . and , corporation between uninhabited combat air vehicle ( ucav ) and as missile is discussed in the process 本文主要针对无人机对地攻击任务特点，开展仿真模型研究，并以此为基础设计出无人机防区外攻击的典型动作链，对攻击过程中无人机与空地导弹的配合问题进行了初步的研究。
During the last phase of auto - landing of shipborne uav ( unmanned air vehicle ) on deck , to make the uav identify and track , and finally fly into the intercept net fixed on the rear deck of naval ship placidly and accurately , it should be consider the influence of deck on landing 舰载无人机在最后着舰回收阶段,为了导引无人机平稳、准确地飞入安装在舰艇尾部甲板上的拦截网中,实现撞网回收,要考虑舰艇因海浪引起的舰体颠簸运动对着舰引导系统的影响。
In modem war , a precise orientation and emendation system applied to artillery spying is needed , existing orientation and emendation system usually computes position of object according uav ( unmanned air vehicle ) ' s position and pose and the pose of vidicon on uav , but orientation is n ' t enough precise 现代战争中需要高精度的炮兵侦察定位校射系统，然而现有的定位校射系统通常是根据无人机的位置、姿态信息和机载摄像机的姿态信息来估计目标区域的位置，定位精度不高。
This paper presents the results of studies on collectivity scheme and some key technologies about the network - based navigation system which is composed by existing stations ( e . g . radio beacon ) , unmanned air vehicles ( e . g . relay uav ) , other air - tactical serving vehicles and data relay satellites 本文研究了利用地面现有台站(如无线电信标台)和移动站(如移动指挥车辆) 、空中无人机平台(如中继无人机)和其他空中战术服务平台、以及数据中继卫星等构成的网络化导航系统的总体方案和相关技术。
The uav ( unmanned air vehicle ) is playing an more and more important role in modern wars . it is featured by long endurance , large cruise range , heavy overload capability as well as attitude alteration limitless and casualty avoid when flying in hostile territory compared to manned air vehicle . compared to satellites it has low altitude , controllable movement , convenient arrangement and low cost 无人机在现代战争中扮演着越来越重要的角色，与有人驾驶飞机相比，无人机机动性能好，过载能力强，不存在飞行员伤亡；与侦察卫星相比，无人机飞行高度低，活动范围可控，部署方便，造价低廉，目前各国都在积极研制各种新型无人机。
The target of this thesis is to develop a design and optimization tool for airfoils of wind - in - ground air vehicle . the functions of the tool include : to generate wing - in - ground air vehicle airfoil by relative less control points , to simulate the wing - in - ground effect by the mirror method , to analyze aerodynamic performance of the airfoil using the software javafoil and to optimization the airfoil by the based - surrogate optimization method 该软件具有如下特点:给出较少的控制点生成一个地效飞行器翼型;采用镜像法来模拟地面效应,应用可以计算地面效应的翼型分析软件javafoil对地效飞行器翼型的空气特性进行分析;应用基于代理模型的优化方法对地效飞行器翼型进行优化。
