波音公司还进行了大量的飞行试验计划，以验证系统的设计与开发。
Boeing also performed an extensive flight-test program to validate the system's design and development.
多年来，美国中途导弹防御系统的开发已经饱受缺乏飞行试验的困扰，部分原因是由于系统复杂性所产生的故障。
The development of the midcourse missile defense system has been plagued by gaps in flight testing over the years due in part to breakdowns resulting from the sheer complexity of the system.
测试验证了垂直飞行所需的所有系统功能运作，并测量STOVL系统运行时飞机安装力量和时间。
The testing demonstrates functional operation of all systems required for vertical flight, and measures the installed forces and moments on the aircraft during STOVL operations.
下一步，BAE系统公司将在美国陆军的测试和评估中对ATRICM和通用导弹预警系统(CMWS)进行飞行试验，以校验这两种系统的性能。
BAE Systems will next conduct a series of flight tests to verify the performance of ATIRCM and the company's Common Missile Warning System (CMWS) in advance of Army test and evaluation.
飞机控制系统的每一个零件都进行过充分的试验。所以请安心坐下，享受你的飞行乐趣，因为不会出什么毛病。
Every part of the aircraft-control system has been fully tested. So, sit back and enjoy your flight since nothing can go wrong.
系统联试和飞行试验证明，该分析方法是可行的。
The system united test and flight test show the feasibility of the analyzing method.
通过试验，选择了合适的结构滤波器参数，有效地抑制了飞行控制系统与飞机弹性结构之间的耦合。
Through ground test, suitable parameters of the structural filter are selected and the coupling between the flight control system and the aircraft elasticity structure is effectively restrained.
介绍“微波空间定位系统(KDCC)”及其在飞行试验中的应用。
This paper introduces a microwave space position system called KDCC and its application in flight test.
该系统经飞行试验证明，性能稳定，工作可靠。
For this system, stable performances and reliable operation have been proved in flight test.
介绍了K8V 变稳飞机飞行试验验证系统的组成及功能。
The configuration and function of the flight testing validation system for the K8V variable stability aircraft are introduced in this paper.
在实际弹丸飞行姿态测试试验中，该测试系统可以较好的完成实时测试小弹丸攻角和速度参数的任务。
In the experiment for measuring bullet attitude, this measurement system can accomplish real-time measuring small bullet Angle of attack and velocity parameter.
分析了飞行试验测试系统的发展趋势。
本文首先介绍了无人机飞控系统的设计过程，采用模型飞行试验进行控制律参数设置与确定。
Firstly, the paper introduce the process of design the UAV AFCS, which use the test of model fly to confirm the control principle parameter.
并且此系统经历了新型火箭飞行试验，通过发射卫星，又取得了入轨精度的验证。
It has undergone new type rocket flight test, and gained high orbit injection accuracy in satellite launching.
在理论和试验上验证了光学引导系统跟踪机动飞行目标的优越性。
The advantage of optical guiding system used in the mobile aero-target tracking is proved in theory and test.
在小子样情况下，利用系统和分系统试验数据对导弹的飞行可靠性指标进行评定，从数学上说是系统可靠性综合问题。
In the situation of small samples, it belongs to systems reliability integration by math that we estimate the flight reliability of missile using systems and subsystems testing data.
该系统已成功地完成了安全飞行试验，并获得批准于今年夏天作为首个任务系统装备F - 35飞机。
The system has successfully completed safety of flight tests and obtained approval for flying this summer onboard the first mission systems equipped F-35 aircraft.
掠海导弹飞行模拟靶标是完成近程反导舰炮武器系统研制试验及装备交验所必须的重要靶标之一。
Flying simulated drone of skimming sea missile is one of the important drone to complete short range antimissile warship gun weapon system development test and equipment adopt.
在详细分析了军事航空监视的系统结构和工作流程的基础上，设计了真实飞行搭载试验的演示验证方案并进行了相关试验。
On the basis of the system architecture and working flow of military aviation surveillance, a verifying solution is planned and associated experimentation is conducted on a real carrying flight.
所研制的系统在Y - 12遥感飞机上进行了搭载飞行试验，获得了符合要求的图像。
The system was tested in Y-12 remote-sensing airplane, and the eligible image was acquired.
这架试验机上安装有我国第一套数字式气动变稳飞行控制系统，这类飞机上不允许地面共振现象存在。
It is not allowed that construction resonance phenomena appear in the aircraft which is equipped with digital variable stability system.
为克服由于试验或飞行数据不足而无法获取系统足够故障模式的问题，开展了液体火箭推进系统故障过程建模与计算机仿真研究工作。
To overcome the difficulties on acquiring enough fault modes from ground and flight test data, the failure process for liquid propellant rocket propulsion systems was modeled.
在直升机飞行控制系统、尤其是控制增稳系统的地面仿真试验中，实施标准的、具有可重复性的杆操纵非常重要。
It is important but difficult to establish uniform and repeatable stick inputs in ground-based simulated experiments of flight control system, especially of stability and control augmentation system.
本文测试了低空大速度飞行试验条件下飞行紧张因素对飞行员呼吸系统的影响。
The effects of the mental tense factor in high speed flight tests at lower altitude on pilots respiratory system are reported in this study.
本文结合某型飞机燃油系统结冰试验技术攻关工作，研究飞机燃油系统结冰飞行试验的燃油配水方法和试验程序。
This paper describes specific fuel setting method and test procedure for airplane fuel system icing flight test which is verified in icing test technology research of an airplane fuel system.
本文依据飞行模拟器对其运动模拟系统运动性能的要求，对飞行模拟试验样机电控部分进行了改造。
In accordance with flight simulator's demand of motion simulation system motion performance, the electro-control part of flight simulation test prototype is reconstructed in this paper.
启动空间飞行器在轨服务与维护系统建设，利用多种资源，开展新原理、新技术、新产品在轨试验验证。
It plans to build in-orbit servicing and maintenance systems for spacecraft and make in-orbit experiments on new theories, technologies and products by tapping various resources.
仿真结果表明，与实际飞行试验数据达到非常好的拟合，说明采用六自由度的制导控制系统的数学模型进行设计的正确性。
Numerical simulation results for sample engagement scenarios are given. It shows that simulation results are very close to the actual flight test results. So …
对综合控制软件的任务剖面进行了分解，并给出了软件在系统测试与飞行试验阶段运行可靠度的计算方法。
Then, based on the decomposition of task section plane of general missile control software, the procedures for the operational reliability .
对综合控制软件的任务剖面进行了分解，并给出了软件在系统测试与飞行试验阶段运行可靠度的计算方法。
Then, based on the decomposition of task section plane of general missile control software, the procedures for the operational reliability .
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