Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system

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United States of America Patent

PATENT NO 8473121
APP PUB NO 20100200701A1
SERIAL NO

12765713

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Abstract

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A fly-by-wire control system for an aircraft including detection of pilot induced oscillations and a mobile control unit for such a system. According to the invention, provision is made for the pivotings of the mobile control unit to be damped by a controllable damper controlled by a detector that detects oscillations corresponding to pilot induced oscillations.

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Patent Owner(s)

  • AIRBUS OPERATIONS SAS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Fabre, Pierre Toulousse, FR 28 262
Gautier, Jean-Pierre Toulouse, FR 59 375
Raimbault, Nathalie Toulouse, FR 3 13
Sagansan, Alain Colomiers, FR 3 37

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