Instead , the controlling according to attitude - controlling of the deformation of aerodynamic configuration is new and advance measure , which has great probability to supply the gap in researching of the control technique of mav . this paper aims that three varied configurations of micro air vehicle will be designed and optimized , then their aerodynamic property will be compared and analyzed , and the prototype of mav will be got 本文旨在对各种气动布局的mav进行气动特性比较分析与综合，得出最适合于mav的原型机，在建立一套基于气动外形形变的性能研究环境的基础上，对该原型机进行气动外形形变先进控制策略的探索。
With the progress of aviation science & technology and the requirement of air combat , multi - targets attack and coordination for multiple unmanned air vehicles ( uav for short ) become the trend of development . targets assignment and trajectory generation strategy pose significant technical challenges 随着航空科技的进步和军事斗争需求的牵引，无人机多机协同攻击多目标将成为未来战争的一种重要模式，多架无人机协同攻击多目标中的目标分配和航迹产生是多架无人机协同作战的关键技术。
Due to more and more application of unmanned air vehicles ( uav ) in war , theinteroperabilityand currencybetween uav systems become veryimportant . in 2001 . 04 , thefirstexperimenttocontrolthetake - offandlandingofamericanavy “ predator ” is carriedoutby the tactical control system ( tcs ) , which is developed by america navy . in theexperiment , the launch and recovery , flight control and payload control is finished , and thedata can be received directly from “ predator ” . for investigate the framework , informationcriterionandkeycontroltechniqueoftcs , it ’ snecessarytotesttheprototypeoftcs 随着无人机在战争中越来越多的应用,无人机系统之间的互操作性和通用性变得尤为重要, 2001年4月,美国海军研制的战术控制系统对美海军“捕食者”无人机进行了首次起飞和降落控制试验,试验完成了无人机的发射和回收、飞行控制、载荷控制,并可从“捕食者”飞机直接接收数据。
Unmanned air vehicle ( uav ) plays a very important role in nowadays research . recently , the applied range of the uav has expended into military , civil and scientific research scopes : in military scopes , it can be used to be detectors and monitors , electronic countermeasure , fire guidance , war evaluation , target simulation etc ; in civil scopes , it can be used to geodetic survey , detect urban environment , survey globosity resource , prevent forest - fire , pretend environment and succor disaster etc ; in scientific research scopes , it can be used to survey and research atmosphere , also it can validate new technology and now facility 随着时代的发展,无人机在社会的各个领域起着越来越重要的作用,近年来,无人机的使用范围已拓展至军事、民用和科研三大领域:在军事上,可用于侦察监视、电子对抗、火力制导、战果评估、目标模拟等;在民用上,可用于大地测量、地球资源勘测和森林防火、环境保护与灾害救援等;在科研上,可用于大气研究、气象观测、新技术新设备的试验验证等。
In the first part , human - machine interface design of ucav ( unmanned combat air vehicle ) is studied . the design criterion of display , controller and working environment for human in ucav system is presented . in the second part , based on the analysis of human error cause , human generic error model is presented 论文的第一部分研究无人作战飞机系统的人机界面设计，论文给出了无人作战飞机系统的功能框图，根据无人机的任务剖面，综合功效学的研究成果，给出了无人机系统的显示装置、控制装置、工作环境和操作人员的组织情况等的设计准则。
Abstract : some problems about overall design of a small unmanned air vehicle telemetry system are presented in this paper . the construction and fundamental principle of the telemetry system is simply introduced . according to the telemetry task requirement , the key problems which should be solved at first are demonstrated mainly by system " s capacity design and channel design . the needed data transmission rate is carefully calculated with the telemetry parameter table provided by user and on this basis the frame structure is decided . the bit error rate in factual telemetry channel is grossly estimated in theory and a channel encoding scheme is provided to improve data transmission quality to meet with the requirement for extremely low bit error rate 文摘:论述了某型号无人机遥测系统中的容量和信道设计问题.文中对该遥测系统的组成和原理进行了介绍.结合具体的遥测任务需求，在容量设计中确定了数据传输率和使用的帧格式，在信道设计中，通过计算实际信道中的误码率，提出了相应的信道编码方案以确保数据传输的低误码率要求
Abstract : a characteristic of piezoresistive pressure sensor and some parameters used to compute altitude and velocity in unmanned air vehicle ( uav ) are introduced . the sensor ' s temperature characteristic is further improved after temperature compensation , it has achieved a satisfactory result by using single chip processor to compute altitude and velocity . the application prospect of the piezoresistive pressure sensor is analysed 文摘:主要介绍了压阻式压力传感器的特点及在无人机上用其来解算高度、速度等参数的使用情况，经过温度补偿后，使传感器的温度特性得到了进一步的改善，用单片机解算高度、速度，达到了满意的效果，同时分析了压阻式传感器的应用前景。
On the base of the soft about the deformation of aerodynamic configuration of mav , the advanced controlling technique of the deformation o f aerodynamic configuration about the prototype mav will be explored . based on the characteristic of micro air vehicle , this paper abstracted the aerodynamic evaluation mathematics models , developed a aerodynamic engineering estimation program , all kinds of aerodynamic configuration was compared and analyzed , found the perfect configuration and got the prototype of mav . abstracted the model about the deformation of aerodynamic configuration on base of the method of vortex lattice , developed the program for researching the performance of the deformation of aerodynamic configuration 本文针对mav的具体特点，抽象出mav的气动工程计算数学模型，建立起气动工程估算环境，对各种气动布局进行了气动特性比较分析与综合，寻求出理想的mav气动布局方案并提出mav原型机，抽象出基于涡格法的气动外形形变的数学模型，建立起气动外形形变性能研究环境，探讨新型的飞行控制方法和气动力控制策略，在得出气动外形形变模型的初始方案后，对其进行进一步的优化，最后得出理想的气动外形形变执行机构组合阵列。
