G - Physics – 05 – D
Patent
G - Physics
05
D
G05D 1/12 (2006.01) B64C 13/50 (2006.01) F41G 3/22 (2006.01) F41G 5/18 (2006.01) F41G 9/00 (2006.01) G05D 1/08 (2006.01)
Patent
CA 2144453
During operation of a flight control system in a coordinated area bombing mode, one pair in a group of pairs of fire control azi- muth coordinate error signal and elevation coordinate error signals (145) are faded-in as the aircraft yaw attitude reference and pitch attitude reference, respectively. Each pair is respectively indicative of the change in aircraft yaw atti- tude and pitch attitude for an air- craft reference axis to be aligned with an aiming line of sight. The aiming line of sight corresponds to a target location within a selected target area. A firing signal (685) is provided in response to both the azimuth and elevation coordinate error signals being below respec- tive threshold magnitudes, and the next pair in the group of pairs of azimuth and elevation coordinate error signals provide the aircraft attitude reference. A selected wea- pon is fired in response to the firing signal.
Fowler Donald W.
Lappos Nicholas D.
Ogilvy Renault Llp/s.e.n.c.r.l.,s.r.l.
United Technologies Corporation
LandOfFree
Helicopter integrated fire and flight control having... does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Helicopter integrated fire and flight control having..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Helicopter integrated fire and flight control having... will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1354968