Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Patent
1998-07-06
2000-01-25
Eldred, J. Woodrow
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
244 60, 180337, 180338, B64C 1134
Patent
active
060169931
ABSTRACT:
The method includes the steps of: acquiring a signal from an acceleration sensor; calculating the Hilbert transform of the signal filtered and sampled beforehand; defining a complex signal having the filtered and sampled signal as the real part and the Hilbert transform of the filtered and sampled signal as the imaginary part; calculating a phase signal given by the difference between the phase of the complex signal and a reference phase; calculating the variance of the phase signal; comparing the variance with at least one predetermined threshold; and generating an alarm signal if the variance exceeds the threshold value.
REFERENCES:
patent: 3699806 (1972-10-01), Weichbrodt
patent: 4654836 (1987-03-01), Wason
patent: 5210704 (1993-05-01), Husseiny
patent: 5344101 (1994-09-01), Francois
patent: 5365787 (1994-11-01), Hernandez et al.
Bellazzi Alberto
Maino Bruno
Eldred J. Woodrow
Finmeccanica S.P.A.
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