Aircraft control system

Aeronautics and astronautics – Aircraft control – Automatic

Reexamination Certificate

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Details

C244S075100, C701S003000, C701S009000, C701S010000

Reexamination Certificate

active

06986486

ABSTRACT:
This invention control system having: means (12) for detecting an irregularity in aircraft handling during flight; means (18) for causing temporarily a rigid body excitation in at least a portion of the aircraft; means (20) for monitoring an actual response to the excitation; means (22) for comparing the actual response and a target response to the rigid body excitation; and means (14) responsive to an output from the comparison means for determining the need for a modification of the current flight plan and for generating a corresponding control output. The invention also provides a corresponding method for controlling an aircraft.

REFERENCES:
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patent: 3074385 (1963-01-01), Nass
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patent: 5186416 (1993-02-01), Fabre et al.
patent: 5819188 (1998-10-01), Vos
patent: 6622972 (2003-09-01), Urnes et al.
patent: 55077/90 (1991-01-01), None
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patent: 0 067 548 (1982-12-01), None
patent: 2 234 353 (1991-01-01), None
patent: 2 267 470 (1993-12-01), None
patent: 9249199 (1997-09-01), None
Patent Abstracts of Japan, vol. 014, No. 147, Mar. 20, 1990, & JP 02 011496 A, Jan. 16, 1990, Abstract.

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