发明授权
US09476989B2 Vector tracking loop operability through oscillator micro-jump event
有权
通过振荡器微跳事件的矢量跟踪环路可操作性
- 专利标题: Vector tracking loop operability through oscillator micro-jump event
- 专利标题(中): 通过振荡器微跳事件的矢量跟踪环路可操作性
-
申请号: US14254285申请日: 2014-04-16
-
公开(公告)号: US09476989B2公开(公告)日: 2016-10-25
- 发明人: James B. Broderick , Lawrence Charles Vallot
- 申请人: Honeywell International Inc.
- 申请人地址: US NJ Morris Plains
- 专利权人: Honeywell International Inc.
- 当前专利权人: Honeywell International Inc.
- 当前专利权人地址: US NJ Morris Plains
- 代理机构: Fogg & Powers LLC
- 主分类号: G01S19/23
- IPC分类号: G01S19/23 ; G01S19/47 ; G01S19/00
摘要:
A navigation system comprises a GNSS receiver that receives GNSS signals on multiple tracking channels, an INS that generates inertial data, and a processor. A micro jump detection and correction module comprises an oscillator micro jump detector that monitors estimates of C/N0 in all tracking channels, and detects a micro-jump event when there is an abrupt decrease of C/N0 in all tracking channels. An offsets module defines a plurality of carrier NCO command offsets to search over signal Dopplers in all available tracking channels after the micro jump event is detected, and sends the carrier NCO command offsets to the GNSS receiver to be added to nominal carrier NCO commands. The micro jump detector selects a tracking channel with the highest C/N0 after carrier NCO command offsets are added to nominal carrier NCO commands, computes corrections for clock error estimates, and sends the corrections for the clock error estimates to a GNSS/inertial Kalman filter.
公开/授权文献
信息查询