Invention Grant
US08473121B2 Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
有权
一种用于飞行器的线控控制系统，包括检测导频感应振荡和这种系统的控制
- Patent Title: Fly-by-wire control system for an aircraft comprising detection of pilot induced oscillations and a control for such a system
- Patent Title (中): 一种用于飞行器的线控控制系统，包括检测导频感应振荡和这种系统的控制
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Application No.: US12765713Application Date: 2010-04-22
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Publication No.: US08473121B2Publication Date: 2013-06-25
- Inventor: Nathalie Raimbault , Jean-Pierre Gautier , Alain Sagansan , Pierre Fabre
- Applicant: Nathalie Raimbault , Jean-Pierre Gautier , Alain Sagansan , Pierre Fabre
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Dickinson Wright PLLC
- Priority: FR0214388 20021118
- Main IPC: G01C23/00
- IPC: G01C23/00 ; G05D1/00 ; G05D3/00 ; G06F7/00 ; G06F17/00
Abstract:
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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