Helicopter pitch rate feedback bias for pitch axis...

Details Helicopter pitch rate feedback bias for pitch axis... Helicopter pitch rate feedback bias for pitch axis...

B - Operations, Transporting

64

C

244/16

B64C 11/34 (2006.01) B64C 27/54 (2006.01) G05D 1/08 (2006.01)

Patent

CA 1085368

HELICOPTER PITCH RATE FEEDBACK BIAS FOR PITCH AXIS MANEUVERING STABILITY AND LOAD FEEL ABSTRACT OF THE DISCLOSURE The longitudinal cyclic pitch channel of a helicopter has a negative pitch rate feedback bias added thereto when flying at higher speeds, thereby to stabilize the pitch axis against aft-load maneuvering instability and/or to induce a requirement for the pilot to provide a countermanding longi- tudinal cyclic pitch input through his cyclic pitch stick, the normal feel force of which provides an indication to him of the loading of the rotor as a consequence of undergoing pitch rate maneuvers.

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