Integrated elevator and thrust control system for aircraft

Details Integrated elevator and thrust control system for aircraft Integrated elevator and thrust control system for aircraft

B - Operations, Transporting

64

C

B64C 19/02 (2006.01) B64C 13/16 (2006.01) B64C 13/50 (2006.01) B64D 31/06 (2006.01) G05D 1/00 (2006.01) G05D 1/06 (2006.01) G05D 1/10 (2006.01)

Patent

CA 2055089

- Système de commande en profondeur et en poussée pour un aéronef. - Selon l'invention, chacun des ordres de commande en profondeur (.delta.q) et de commande en poussée (.delta..pi.) est une combinaison linéaire, entre autres, de l'assiette et de la vitesse commandées (.theta.c et Vcc) et le pilotage au manche (14) de l'aéronef est réalisé en vitesse de tangage (.theta.c). On peut prévoir des protections en assiette, en incidence et en facteur de charge vertical.

Affiliated with

Also associated with

Rating

Integrated elevator and thrust control system for aircraft 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 elevator and thrust control system for aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Integrated elevator and thrust control system for aircraft will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1964083