Integrated attitude altimeter

Details Integrated attitude altimeter Integrated attitude altimeter

2007-05-10

2009-08-18

Tarcza, Thomas H (Department: 3662)

Communications: directive radio wave systems and devices (e.g.,

Determining distance

Altimeter

C342S094000, C342S121000, C342S176000

Reexamination Certificate

active

07576684

ABSTRACT:
An aircraft electronics system is provided that includes a radar system, a display, an embedded global positioning/inertial navigation system (EGI) and a processor. The radar system is configured to generate aircraft operational data. The display is configured to display the aircraft operational data. The EGI is configured to generate aircraft behavior components and the processor configured to override the aircraft operation data displayed on the display when at least one of the aircraft behavior components is beyond a defined limit, wherein potentially incorrect aircraft operational data affected by at least one of the aircraft behavior component is not displayed.

REFERENCES:
patent: 4431994 (1984-02-01), Gemin
patent: 5410317 (1995-04-01), Ostrom et al.
patent: 5777573 (1998-07-01), Klausing et al.
patent: 6567014 (2003-05-01), Hansen et al.
patent: 6750807 (2004-06-01), Hager et al.
patent: 2003/0210176 (2003-11-01), Hager et al.
patent: 2004/0141170 (2004-07-01), Jamieson et al.
patent: 2005/0179579 (2005-08-01), Pinder et al.

Affiliated with

Also associated with

Rating

Integrated attitude altimeter does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Integrated attitude altimeter, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Integrated attitude altimeter will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-4124674