08214090 is referenced by 3 patents and cites 34 patents.

Disclosed is a method and device for generating a yaw rate command for an aircraft along a ground trajectory. The yaw rate command is generated by determining a current curvature, lateral deviation and angular deviation of the ground trajectory. A yaw rate calculator then calculates a yaw rate and generates the yaw rate command based on the determined current curvature, lateral deviation and angular deviation.

Title
Method and device for generating a yaw speed order for an aircraft during a taxiing
Application Number
12/330372
Publication Number
8214090 (B2)
Application Date
December 8, 2008
Publication Date
July 3, 2012
Inventor
Pierre Scacchi
Toulouse
FR
Fabrice Villaume
Seysses
FR
Agent
Dickinson Wright PLLC
Assignee
Airbus Operations SAS
FR
IPC
G05D 1/00
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