Aircraft navigation using the global positioning system and...

Data processing: vehicles – navigation – and relative location – Navigation – Employing position determining equipment

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C701S220000

Reexamination Certificate

active

08082099

ABSTRACT:
A vehicle navigation technique uses a receiver for signals of a global positioning system to produce a first position indication and a first velocity indication. An attitude and heading reference system employs accelerometers and gyroscopes oriented along three axes. The raw signals from the accelerometers and gyroscopes are used to derive a second position indication and a second velocity value. A Kalman filter function is applied to the first and second position indications and to the first and second velocity indications to thereby produce a present position indication and a present velocity indication. The Kalman filter function exploits GPS data to corrects periodic drift in the position and velocity indications derived form the accelerometers and gyroscopes by calculating accelerometer and gyroscope biases, thereby enabling relatively inexpensive devices to be utilized.

REFERENCES:
patent: 4930085 (1990-05-01), Kleinschmidt
patent: 5216611 (1993-06-01), McElreath
patent: 5375059 (1994-12-01), Kyrtsos et al.
patent: 5512903 (1996-04-01), Schmidtke
patent: 5617317 (1997-04-01), Ignagni
patent: 5631656 (1997-05-01), Hartman et al.
patent: 5672872 (1997-09-01), Wu et al.
patent: 5760737 (1998-06-01), Brenner
patent: 6145378 (2000-11-01), McRobbie et al.
patent: 6694260 (2004-02-01), Rekow
patent: 6697736 (2004-02-01), Lin
patent: 7107833 (2006-09-01), Osborne
patent: 7248964 (2007-07-01), Bye
patent: 7400956 (2008-07-01), Feller et al.
patent: 7409290 (2008-08-01), Lin
patent: 7805241 (2010-09-01), Sato
patent: 2002/0158796 (2002-10-01), Humphrey et al.
patent: 2003/0149528 (2003-08-01), Lin
patent: 2005/0007450 (2005-01-01), Hill et al.
patent: 2006/0287824 (2006-12-01), Lin
patent: 2007/0234933 (2007-10-01), Donnell et al.
patent: 2008/0167770 (2008-07-01), Macdonald et al.
patent: 2008/0234933 (2008-09-01), Chowdhary et al.
patent: 2008/0269988 (2008-10-01), Feller et al.
patent: 2009/0091351 (2009-04-01), Bueti et al.
patent: 2009/0099774 (2009-04-01), Takac et al.
patent: 2009/0115656 (2009-05-01), Raman et al.
patent: 2009/0326851 (2009-12-01), Tanenhaus
patent: 2010/0106416 (2010-04-01), Yochum
patent: 2011/0202204 (2011-08-01), Kahn
Schlee, F.H., et al., Use of an External Cascade Kalman Filter to Improve the Performance of a Global Positioning System (GPS) Inertial Navigator, IEEE Proceedings National Aerospace and Electronics Conference, Abstract, May 23-27, 1988, Ohio.
Gebre-Egziabher, D., et al., A Low-Cost GPS/Inertial Attitude Heading Reference System (AHRS) for General Aviation Applications, IEEE Position Location and Navigation Symposium, Apr. 20-23, 1998.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Aircraft navigation using the global positioning system and... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft navigation using the global positioning system and..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft navigation using the global positioning system and... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4299671

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.