首页> 外国专利> GPS PRECISION APPROACH AND LANDING SYSTEM FOR AIRCRAFT

GPS PRECISION APPROACH AND LANDING SYSTEM FOR AIRCRAFT

机译:飞机的GPS精密进场和着陆系统

摘要

A GPS precision approach and landing system for aircraft employs a fixedground facility and a single satellite navigation receiver on board theaircraft. The fixed ground facility includes a reference receiver thatmeasuresdifferential corrections to the satellite code and carrier measurements and apseudolite that is employed to transmit these corrections to a broadband GPSreceiver on board the aircraft and to provide an additional code and carriermeasurement to assist in the navigation solution. The pseudolite signal isbroadcast at a frequency offset from the L1 GPS frequency in order to preventinterference with the satellite navigation system. The broadband GPS receiveron board the aircraft is capable of making phase coherent measurements fromtheGPS satellites, the pseudolite signal, and the GLONASS satellites. These phasecoherent measurements are combined to form a precise differential carrierranging (DCR) solution that is used to provide three-dimensional positionguidance of the aircraft throughout a precision approach and landingprocedure.
机译:用于飞机的GPS精确进场和着陆系统采用固定地面设施和机载单个卫星导航接收器飞机。固定地面设施包括一个参考接收器,措施卫星代码和载波测量的差分校正以及伪卫星,用于将这些校正结果传输到宽带GPS飞机上的接收器,并提供附加代码和承运人测量以协助导航解决方案。伪卫星信号是以与L1 GPS频率偏移的频率广播,以防止干扰卫星导航系统。宽带GPS接收器飞机上可以进行相位相干测量的GPS卫星,伪卫星信号和GLONASS卫星。这些阶段相干测量被组合以形成精确的差分载波测距(DCR)解决方案,用于提供三维位置在整个精确进近和着陆过程中对飞机的制导程序。

著录项

  • 公开/公告号CA2105846C

    专利类型

  • 公开/公告日2002-11-19

    原文格式PDF

  • 申请/专利权人

    申请/专利号CA19932105846

  • 发明设计人 BROWN ALISON K.;

    申请日1993-09-09

  • 分类号G01S5/14;

  • 国家 CA

  • 入库时间 2022-08-21 23:58:56

相似文献

  • 专利
  • 外文文献
  • 中文文献
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