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- Flight Test Interface Unit 飞行测试接口装置
- The inertial measurement unit, gyro, accelerometer and data interface unit etc are also introduced in detail, Finally, thispaper recommends system operation and flight test result. 详细介绍了惯性测量装置、陀螺仪、加速度表、数据接口单元等。 最后介绍了系统工作和飞行试验结果。
- Our TM BUS design is based on two sets of standards: IEEE STD 1149.1 and IEEE STD 1149.5. In section 2.1, we discuss in detail the architecture of our TM BUS. Fig. 2 shows its TIU (test interface unit or test controller). 简要介绍了测试维护总线TM- BUS(test and maintenance bus)及其应用 ,论述设计的 TM- BUS控制器的结构、实现及 TM-BUS控制管理机制。
- Participate in the flight test procedures improvement. 参与试飞程序的完善。
- Research of JL8 aircraft stall and spin flight test is described in this paper. 叙述了JL8飞机失速尾旋试飞状态、试飞方法和试飞结果。
- LXT384is a octal T1/E1/J1line interface unit,which is applied in SONET/SDH. LXT384是一个用于SONET/SDH设备的八进制T1/E1/J1线路接口单元芯片。
- Any flight test and wind tunnel correlation always suffers from a great number of unknowns. 在对飞行试验与风洞试验进行比较时总有大量的未知数。
- And a reserved producing fluid level (PFL) testing interface. 同时预留有动液面测试接口。
- Universal test interface scanner, you can simplify the associated development, and testing. Simple structure, easy to implement and use. 通用的扫描仪测试接口，可以简化相关的开发，及测试。结构简单，容易实现和使用。
- Describe the basic progression of the first flight tests. 请描述一下首飞测试的基本过程。
- The paper build a WBEM_based distributed instrument test system which has the unified management and automatic test interface. 本论文搭建了一个基于WBEM标准的统一的仪器管理和自动测试接口的分布式仪器测试系统。
- This marks the second time the NLOS-LS CLU was used in a flight test of the PAM missile. NLOS-LS为指挥官提供即时、精确响应的火力，打击移动和静止的陆地、海上目标。
- MPC860 consists of three major blocks:the Embedded PowerPC core,the System Interface Unit(or SIU),and the Communications Processor Module(or CPM). MPC860包括三个主要部分：嵌入式PowerPC内核、系统接口单元、通信处理器模块。
- The flight test monitor and command system is main part of flight test engineering. 试飞监控与指挥系统是飞行试验工程中的重要组成部分。
- This paper expounds the method that designs Bus Interface Unit(BIU) by the new techniques, the key unit in MIL-STD-1553B data bus system. 本论文论述了用新技术来设计MIL-STD-1553B总线系统中的关键部件 总线接口单元的设计方法。
- In addition, preliminary proof for the half system flight test program of SITAN algorithm was discussed. 此外还对SITAN系统半 系统试飞方案作了初步的论证工作。
- Finally, according to the ATO's characteristic, the malfunction data display interface unit is designed which has HDLC communication controller. 最后,根据ATO的特点,设计出了带HDLC通信控制器的故障数据显示接口单元。
- The poesend problems in evaluation antiship missile flight test are pcinted out. 指出现行反舰导弹飞行试验结果评定的命中域标准存在的问题。
- This data is then modulated and sent to the Interface Unit, which demodulates the signal and sends it back to the computer. 这个数据，然后调制和发送到接口单元，其中解调信号并传送到计算机。
- Due to the mission at the Air Force Flight Test Center, it operates a great variety of aircraft. 由于在空军班机测试中心的任务，它操作飞机的一个很棒的多样性。
