System and method for optimized runway exiting

Details System and method for optimized runway exiting System and method for optimized runway exiting

2007-07-13

2010-10-19

Tran, Khoi (Department: 3664)

Data processing: vehicles, navigation, and relative location

Vehicle control, guidance, operation, or indication

Aeronautical vehicle

C244S111000, C244S183000, C701S015000, C340S959000

Reexamination Certificate

active

07818100

ABSTRACT:
Methods and apparatus are provided for optimizing runway exiting. Prior to landing, the pilot may choose to input one or more new landing parameters. Then, based on current landing parameters (e.g., any new landing parameter(s) and remaining default landing parameters) and the aircraft performance parameters, predicted landing performance can be updated and indicia of the updated predicted landing performance can be displayed to the pilot on an updated airport map and display. The updated predicted landing performance can include, among other things, a display of AUTOBRAKE landing performance. When no further changes to the current landing parameters are desired, the automatic braking system can be set to provide dynamic braking to slow the aircraft to a selected velocity at a selected position on a particular runway.

REFERENCES:
patent: 5968106 (1999-10-01), DeVlieg et al.
patent: 6112141 (2000-08-01), Briffe et al.
patent: 7014146 (2006-03-01), Villaume et al.
patent: 2002/0077743 (2002-06-01), Schmidt
patent: 2003/0009278 (2003-01-01), Mallet et al.
patent: 2005/0006524 (2005-01-01), Villaume et al.
patent: 2006/0038068 (2006-02-01), Sullivan
patent: 2006/0271250 (2006-11-01), Dubeck et al.
patent: 2007/0021878 (2007-01-01), Builta et al.
patent: 2007/0208466 (2007-09-01), Meunier
patent: 2008/0179452 (2008-07-01), Kinkopf et al.
patent: PCT/US 2008/056877 (2008-03-01), None
(NASA-CR-195026) Guidance and Control Requirements for High-Speed Rollout and Turnoff (ROTO) Final Report (McDonnell-Douglas Aerospace) 127 p Nasa Contractor Report 195026, Contract NAS1-19703 Task 3, Jan. 1995, National Aeronautics and Space Adminstration Langley Research Center, Hampton, VA 23681-0001.

Affiliated with

Also associated with

Rating

System and method for optimized runway exiting does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with System and method for optimized runway exiting, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and System and method for optimized runway exiting will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-4204234