Invention Grant
- Patent Title: Method and system for controlling the flight of an aircraft with respect to the pitch axis
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Application No.: US15096812Application Date: 2016-04-12
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Publication No.: US10023301B2Publication Date: 2018-07-17
- Inventor: Mathieu Carton , Pierre Debusschere , Laurent Albugues
- Applicant: Airbus Operations (SAS)
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1553269 20150414
- Main IPC: G05D1/00
- IPC: G05D1/00 ; B64C13/22 ; B64C13/50 ; B64C13/04 ; G05D1/06
Abstract:
A system including a load factor control module for calculating a deflection order on manual actuation of a control column by a pilot of the aircraft and transmitting that deflection order to at least one elevator of the aircraft, a longitudinal attitude control module for maintaining the longitudinal attitude of the aircraft at a target attitude in the event of absence of manual actuation of the control column by the pilot during a flight, and a transition management module for determining and storing a present longitudinal attitude value of the aircraft at a recording moment and transmitting that longitudinal attitude value to the longitudinal attitude control module for the longitudinal attitude control module to use the longitudinal attitude value as the target attitude.
Public/Granted literature
- US20160304189A1 Method and system for controlling the flight of an aircraft with respect to the pitch axis Public/Granted day:2016-10-20
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