U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Location system and method with acquisition of accurate location parameters

Patent 5515062 Issued on May 7, 1996. Estimated Expiration Date: Icon_subject August 11, 2013. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3742498

3769589

Range determining system
Patent #: 4278977
Issued on: 07/14/1981
Inventor: Nossen

Navigation system and method
Patent #: 4445118
Issued on: 04/24/1984
Inventor: Taylor ,   et al.

Differential Doppler receiver
Patent #: 4453165
Issued on: 06/05/1984
Inventor: Maine

High dynamic global positioning system receiver
Patent #: 4578678
Issued on: 03/25/1986
Inventor: Hurd

Satellite-based position-determining system
Patent #: 4918609
Issued on: 04/17/1990
Inventor: Yamawaki

Method and system for locating an unknown transmitter
Patent #: 5008679
Issued on: 04/16/1991
Inventor: Effland, et al.

Precise satellite ranging and timing system using pseudo-noise bandwidth synthesis Patent #: 5041833
Issued on: 08/20/1991
Inventor: Weinberg

Inventors

Assignee

Application

No. 105227 filed on 08/11/1993

US Classes:

342/457, Land vehicle location (e.g., bus, police car342/352, Including a satellite342/418Doppler

Examiners

Primary: Issing, Gregory C.

Attorney, Agent or Firm

International Classes

G01S 003/02
G01S 003/52
H04B 007/185

Abstract

A location system relies upon a non-coherent, FDM/TDM communication scheme to measure location parameters. A locator unit moves relative to the locatable unit. A series of messages are communicated between the locator unit and the locatable unit. Through feedback provided from the locator unit to the locatable unit, the locatable unit adjusts its reference frequency and time base so that signals it transmits arrive at the locator unit on a desired frequency and at a desired time slot. The locatable unit estimates Doppler and propagation duration and transmits the estimates to the locator unit. The locator unit measures offsets between desired frequencies and time slots and actual frequencies and time slots. The offsets are combined with the locatable unit's estimates of Doppler and propagation duration to form an integrated Doppler parameter and an integrated propagation duration parameter. The integrated Doppler and propagation duration are used to determine location.

Other References

  • "Emitter Location Accuracy Using TDOA and Differential Doppler" by Paul C. Chestnut from IEEE Transactions on Aerospace and Electronic Systems, vol. AES-18, No. 2, Mar. 1982
  • "Geolocation of Frequency-Hopping Transmitters via Satellite" by A. Sonnenschein and W. K. Hutchinson from Technical Report 900, Nov., 1990
  • "Geolocation via Satellite: A Methodology and Error Analysis" by M. J. Shensa from Technical Report 1244, May 198
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