Method and device for piloting an aircraft optimizing the...

Aeronautics and astronautics – Aircraft control – Rudders and empennage

Reexamination Certificate

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C244S195000

Reexamination Certificate

active

08083178

ABSTRACT:
In conformance with the invention, based on the incident conditions and velocity, the steering of the ailerons is weakly negative (b0) or corresponds either to the maximum sharpness of the aircraft (b1), or the optimal lift of the latter (b2).

REFERENCES:
patent: 2210642 (1940-08-01), Thompson
patent: 2407401 (1946-09-01), Clauser
patent: 3734432 (1973-05-01), Low
patent: 4455004 (1984-06-01), Whitaker, Sr.
patent: 4479620 (1984-10-01), Rogers et al.
patent: 4705236 (1987-11-01), Rudolph
patent: 6970773 (2005-11-01), Phillips
patent: 7243881 (2007-07-01), Sakurai et al.
patent: 7494094 (2009-02-01), Good et al.
patent: 0 075 966 (1983-04-01), None
patent: 2 425 379 (1979-12-01), None
International Search Report dated Sep. 6, 2007 w/ English translation.
Written Opinion of the International Searching Authority with English translation.

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