• 主题
高级搜索  >
历史搜索 清空历史
首页> 外国专利> CHANNEL FOR MEASUREMENT OF ANGULAR VELOCITIES OF AIRCRAFTS WITH MULTIFUNCTIONAL LONGITUDINAL MODE SELECTOR AND INCREASED CAPABILITIES FOR LASER INFORMATION AND MEASURING SYSTEM OF A LAUNCH-SITE TEST COMPLEX

CHANNEL FOR MEASUREMENT OF ANGULAR VELOCITIES OF AIRCRAFTS WITH MULTIFUNCTIONAL LONGITUDINAL MODE SELECTOR AND INCREASED CAPABILITIES FOR LASER INFORMATION AND MEASURING SYSTEM OF A LAUNCH-SITE TEST COMPLEX

机译：具有多功能纵向模式选择器的航空器角速度的测量通道和发射场测试复合体的激光信息和测量系统的能力增强

页面导航
  • 摘要
  • 著录项
  • 相似文献

摘要

A channel for measurement of angular velocities of aircrafts with multifunctional longitudinal mode selector and increased capabilities for laser information and measuring system of a launch-site test complex includes a control element, a block for control of deflectors, pumped laser, multifunctional longitudinal mode selector, block of deflectors, transmitting optics, receiving optics, photo-detector, broadband amplifier, information block with increased capabilities with b input of signal of tangent component of velocity (angular velocities) of the aircraft that is measured, resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, triggers "1"|"0", circuits AND, reversible counters, comparison circuits (CC) and - input of reference signals with frequencies of inter-mode beats (23, 6) from transmitting laser. After CC instead of electronic-digital computing machine a computer is included.
机译：带有多功能纵向模式选择器的飞机角速度测量通道，以及增强的激光信息和发射场测试综合体测量系统的功能的通道，包括控制元件，用于偏转器的控制块，泵浦激光，多功能纵向模式选择器，偏转器模块，发射光学器件，接收光学器件，光电探测器，宽带放大器，具有增强功能的信息模块，其中b是所测量的飞机速度的切线分量（角速度）的信号输入，谐振放大器已调整为相应的频率模式间节拍，脉冲形成器，触发器“ 1” |“ 0”，电路“与”，可逆计数器，比较电路（CC），以及-来自发射激光器的具有模式间节拍（23、6）频率的参考信号的输入。在CC之后而不是电子数字计算机中，包括一台计算机。

著录项

相似文献

  • 专利
  • 外文文献
获取专利

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

  • 客服微信

  • 服务号