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
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N/A
Issued Date -
Jan 27, 2005
app pub date -
Nov 10, 2003
filing date -
Nov 18, 2002
priority date (Note) -
Abandoned
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Abstract
Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system. According to the invention, provision is made for the pivotings of said control (2) to be damped by controllable damping means (15, 16) controlled by means (7) detecting oscillations corresponding to pilot induced oscillations.
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