Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Patent
1987-06-26
1988-05-03
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
B64C 2757
Patent
active
047415010
ABSTRACT:
Collective stick inputs are provided (18) to a high pass filter (24) when collective stick reversals in excess of a threshold collective authority rate (15%/sec) and in excess of a threshold frequency (3 stick reversals per second) are sensed. The output of the high pass filter (24) is scaled (26) and subtracted (14) from the collective inputs so as to effectively cancel the threshold stick reversals. Otherwise, if no stick reversals in excess of the threshold collective authority rate are sensed for a threshold time interval (5 seconds), the collective stick inputs are not provided to the high pass filter.
REFERENCES:
patent: 3756543 (1973-09-01), Fowler et al.
patent: 3833189 (1974-09-01), Fowler et al.
patent: 4279391 (1981-07-01), Adams et al.
Clelford Douglas H.
Murphy Richard D.
Tefft Franklin A.
Corl Rodney
Peters Jr. Joseph F.
United Technologies Corporation
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