公开(公告)号：US06781513B1

公开(公告)日：2004-08-24

申请号：US09561576

申请日：2000-04-28

申请人： Richard August Korkosz ,  John Erik Hershey ,  William Robert McKinney, Sr. ,  Bruce Gunter Schings ,  Harold Woodruff Tomlinson, Jr. ,  Charles McDonald Puckette ,  Naofal Mohammed Wassel Al-Dhahir ,  John Anderson Fergus Ross

发明人： Richard August Korkosz ,  John Erik Hershey ,  William Robert McKinney, Sr. ,  Bruce Gunter Schings ,  Harold Woodruff Tomlinson, Jr. ,  Charles McDonald Puckette ,  Naofal Mohammed Wassel Al-Dhahir ,  John Anderson Fergus Ross

IPC分类号： G08B108

CPC分类号： H04B7/18506 ,  G08C15/12 ,  G08C17/02 ,  H01Q1/241 ,  H01Q1/246 ,  H01Q1/28 ,  H01Q1/32 ,  H01Q1/3233 ,  H01Q3/2605

摘要： A telemeter for telemetry of diagnostic messages from a mobile asset to a remote station comprises a processor coupled to the output of one or more condition sensors. The processor converts the output of the condition sensors to a diagnostic message, and provides the diagnostic message at a processor output. A transmitter is coupled to the processor output. The transmitter is adapted to transmit the diagnostic messages in the Industrial, Scientific, Medical (ISM) frequency band. An exemplary embodiment of a telemetry system of the invention comprises a telemeter adapted to transmit diagnostic messages in the ISM frequency band, and a remote station including a receiver for receiving the diagnostic messages in the ISM band.

摘要翻译： 用于从移动资产到远程站的诊断信息遥测的遥测器包括耦合到一个或多个状态传感器的输出的处理器。 处理器将条件传感器的输出转换为诊断消息，并在处理器输出端提供诊断消息。 发射机耦合到处理器输出。 发射机适用于在工业，科学，医疗（ISM）频段发送诊断信息。 本发明的遥测系统的示例性实施例包括适于在ISM频带中发送诊断消息的远程计量器，以及包括用于在ISM频带中接收诊断消息的接收机的远程站。

公开(公告)号：US06426720B1

公开(公告)日：2002-07-30

申请号：US09541545

申请日：2000-04-03

申请人： John Anderson Fergus Ross ,  John Erik Hershey ,  Richard August Korkosz ,  Naofal Mohammed Wassel Al-Dhahir ,  William Robert McKinney ,  Bruce Gunter Schings

发明人： John Anderson Fergus Ross ,  John Erik Hershey ,  Richard August Korkosz ,  Naofal Mohammed Wassel Al-Dhahir ,  William Robert McKinney ,  Bruce Gunter Schings

IPC分类号： H01Q322

CPC分类号： G08C15/12 ,  G08C17/02 ,  H01Q1/241 ,  H01Q1/246 ,  H01Q1/28 ,  H01Q1/32 ,  H01Q1/3233 ,  H01Q3/2605 ,  H04B7/18502 ,  H04B7/18506

摘要： A system for directing a receiving lobe of an adaptive antenna array toward an aircraft in flight includes an aircraft position vector calculator and an antenna weight vector generator. The aircraft position vector calculator receives aircraft position information from an aircraft tracking service and calculates, based upon the aircraft position information it receives, an aircraft position vector g. An antenna weight vector generator receives the aircraft position vector g from the aircraft position vector calculator and generates, based upon the aircraft position vector g, an antenna element weight vector w. The antenna weight vector w is applied to the elements of an adaptive antenna array to direct a receiving lobe of the array towards an aircraft in flight.

摘要翻译： 用于将自适应天线阵列的接收波瓣引导到飞行中的飞行器的系统包括飞行器位置矢量计算器和天线加权矢量发生器。 飞行器位置矢量计算器从飞机跟踪服务器接收飞机位置信息，并且基于其接收到的飞行器位置信息来计算飞行器位置矢量g。 天线权重向量生成器从飞行器位置矢量计算器接收飞机位置矢量g，并且基于飞机位置向量g生成天线元重量向量w。 天线权重向量w被施加到自适应天线阵列的元件，以将阵列的接收波瓣引向飞行中的飞行器。

公开(公告)号：US06628995B1

公开(公告)日：2003-09-30

申请号：US09637441

申请日：2000-08-11

申请人： Shannon Lee Korson ,  Bruce Gunter Schings ,  Packey Pasquale Velleca ,  Mary Beth Golding

发明人： Shannon Lee Korson ,  Bruce Gunter Schings ,  Packey Pasquale Velleca ,  Mary Beth Golding

IPC分类号： G05B2102

CPC分类号： G01D9/005 ,  Y10S244/904

摘要： Aircraft flight data collection is enhanced by changing the data sampling rate as a function of an operational condition of the aircraft, such as its flight phase. An algorithm is used to determine the flight phase. Then, the data is collected at a first sampling rate when the flight phase is one of a first set of flight phases and collected at a second sampling rate when the flight phase is one of a second set of flight phases. The second sampling rate is greater than the first sampling rate to maximize the data storage capacity of the system. Generally, the higher sampling rate is used with transient flight phases such as takeoff and thrust reverse.

摘要翻译： 通过改变作为飞机运行状态的函数（如飞行阶段）的数据采样率来增强飞行器飞行数据采集。 使用算法来确定飞行阶段。 然后，当飞行阶段是第一组飞行阶段之一并且当飞行阶段是第二组飞行阶段之一时以第二采样率收集时，以第一采样率收集数据。 第二采样率大于第一采样率，以最大化系统的数据存储容量。 一般来说，较高的采样率与起飞和推力相反的瞬态飞行阶段一起使用。