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

Relative guidance using the global positioning system

Patent 5344105 Issued on September 6, 1994. Estimated Expiration Date: Icon_subject September 21, 2012. 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

Method and apparatus for aiming artillery with GPS NAVSTAR
Patent #: 4741245
Issued on: 05/03/1988
Inventor: Malone

Portable target locator system
Patent #: 4949089
Issued on: 08/14/1990
Inventor: Ruszkowski, Jr.

Apparatus and method for remote guidance of cannon-launched projectiles Patent #: 5131602
Issued on: 07/21/1992
Inventor: Linick

Inventor

Application

No. 947623 filed on 09/21/1992

US Classes:

244/3.14, Radio wave342/62Missile or spacecraft guidance

Examiners

Primary: Lobo, Ian J.

Attorney, Agent or Firm

International Class

F41G 007/28

Abstract

A method for guiding a vehicle (30) to a target (28) includes furnishing a first vehicle (20) having a first global positioning system (GPS) receiver (24) fixed to receive global positioning signals from a selected constellation (46) of satellites in orbit above the earth and the second vehicle (30) having a second GPS receiver (32) fixed to receive global positioning signals from the same selected constellation (46) of GPS satellites. The first vehicle (20) locates the target (28) with an onboard sensor (26) and converts the location of the target (28) to the frame of reference of the selected constellation (46) of satellites of the GPS. The first vehicle (20) communicates this target position and the available set of GPS satellites to a navigation system of the second vehicle (30). The second vehicle (30) proceeds to the target location provided from the first vehicle (20 ) in the frame of reference of the GPS under control of its navigation system using the positioning signal derived from the second GPS receiver (32) fixed to receive positioning signals from the selected constellation (46) of satellites. In these operations, the second vehicle (30) remains within a sufficiently small operating distance of the position of the first vehicle (20) that variations in systematic bias errors between the first GPS receiver (24) and the second GPS receiver (32) are negligible.

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