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

Method and apparatus for maximum likelihood estimation direct integer search in differential carrier phase attitude determination systems

Patent 5296861 Issued on March 22, 1994. Estimated Expiration Date: Icon_subject November 13, 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

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Inventor: Pentheroudakis

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Inventor: Malone

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Method for precision dynamic differential positioning
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Inventor: Hatch

Method and system for determining position from signals from satellites
Patent #: 4870422
Issued on: 09/26/1989
Inventor: Counselman, III

Apparatus for and a method of determining compass headings
Patent #: 4881080
Issued on: 11/14/1989
Inventor: Jablonski

More ...

Inventor

Assignee

Application

No. 976174 filed on 11/13/1992

US Classes:

342/357.11Attitude determination

Examiners

Primary: Blum, Theodore M.

Attorney, Agent or Firm

International Classes

H04B 007/185
G01S 005/02

Abstract

A method for comparing the relative phase of carrier signals received from GPS satellites to determine the roll, pitch and azimuth attitude of ships, aircraft, land vehicles, or survey instruments, accomplishes a maximum likelihood estimation (MLE) optimum solution over the full range of integers and vehicle attitudes. The problem is formulated as an MLE optimization, where vehicle attitude and integers are regarded as parameters to be adjusted to maximize probability of first-difference carrier phase measurements that are actually generated by hardware. Formulation results in weighted-fit error W as the objective criterion to minimize. A Kalman filter is introduced, having same objective criterion. Minimizing computation in Kalman filter leads to a decision tree for the integers. Two ways are shown to prune decision tree. The first is to exclude impossible combinations, such as those that produce an antenna upside down. The second is to generate a lower bound for W at each branch of the tree. A running sum is kept at each stage moving down the tree. When that sum exceeds a reasonableness bound or the current best W found elsewhere in the search, it is guaranteed that all subsequent integer combinations further down the current branch will produce a larger W and the remainder of the current branch can be cut off, speeding up the search.

Other References

  • Cohen and Parkinson, "Mitigating Multipath in GPS Based Attitude Determination," paper at 14th AAS Guidance and Control Conference, Feb. 2-6,. 1991, Keystone, Colo
  • Ron Brown, "A GPS Receiver with Built-In Precision Pointing Capability," paper at the IEEE Position Location and Navigation Symposium (PLANS '90) Las Vegas, Nev., Mar. 1990
  • Rath and Ward, "Attitude Estimation Using GPS," ION National Technical Meeting, San Mateo, Calif. Jan. 1989
  • Nesbo and Canter, "GPS Attitude Determination for Navigation," GPS World, Sep./Oct. 1990, pp. 36-41
  • Patrick Hwang, "A Near-Instantaneous Initialization Method for Attitude Determination," unknown publication, pp. 661-669
  • Ferguson et al., "Three-Dimensional Attitude Determination with the Ashtech 3DF 24-Channel GPS Measurement System," unknown pub
  • Keierleber et al., "Attitude Determination for Space Transfer Vehicles Using GPS," unknown pub
  • Satz et al., "GPS Inertial Attitude Estimation via Carrier Acc . . . ," paper at Institute of Navigation (ION), National Technical Meeting, Phoenix, Ariz., Jan. 22, 1991
  • Ron Hatch, "Instantaneous Ambiguity Resolution," paper presented at KIS Symp., Banff, Canada Sep. 1990
  • Ron Hatch, "Ambiguity Resolution in the Fast Lane," unknown pub., pp. 45-50
  • Burgett, et al., "The Devel. and Apps. of GPS Determined Attitude," paper for NTC '83, Nov. 198
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