Patent application number | Description | Published |
20090314900 | METHOD AND DEVICE FOR REDUCING ON AN AIRCRAFT THE EFFECTS OF A VERTICAL TURBULENCE - The device ( | 12-24-2009 |
20100070114 | METHOD AND DEVICE FOR REDUCING ON AN AIRCRAFT LATERAL EFFECTS OF A TURBULENCE - A method and device for attenuating on an aircraft lateral effects engendered by a turbulence. | 03-18-2010 |
20100292872 | METHOD AND DEVICE FOR AUTOMATICALLY DETECTING A LATERAL DISSYMETRY OF AN AIRCRAFT - The device ( | 11-18-2010 |
20110022251 | METHOD AND DEVICE FOR AIDING THE LATERAL CONTROL OF AN AIRCRAFT DURING AN APPROACH PHASE - An assistance method and device for lateral control of an aircraft upon an approach phase is disclosed. The device ( | 01-27-2011 |
20110029159 | METHOD AND DEVICE FOR REDUCING ON AN AIRCRAFT LATERAL EFFECTS OF A TURBULENCE - A method and device for reducing on an aircraft lateral effects of a turbulence. The device ( | 02-03-2011 |
20110046823 | PROCESS AND DEVICE FOR OPTIMISING THE PERFORMANCE OF AN AIRCRAFT IN THE PRESENCE OF A LATERAL DISSYMETRY - A process and device for optimising the performance of an aircraft in the presence of a lateral dissymmetry is disclosed. The device ( | 02-24-2011 |
20110071710 | METHOD AND DEVICE FOR DETECTING AN ERRONEOUS SPEED GENERATED BY AN AIR DATA INERTIAL REFERENCE SYSTEM - Method and device for detecting an erroneous speed generated by an air data inertial reference system. The device ( | 03-24-2011 |
20110172853 | METHOD AND DEVICE FOR ATTENUATING THE EFFECTS OF TURBULENCE ON AN AIRCRAFT - A method for attenuating effects of turbulence on an aircraft, and a device to implement the method, the method including: using at least one signal on a wind profile signal, along an excitation direction, representing, at a given moment in an aircraft referential, a component along the excitation direction of the wind speed at a front of the aircraft according to a distance along a longitudinal direction of the aircraft; carrying out a frequency determination, in which the wind profile signal is processed to determine a frequential content; and selecting a control strategy to be adopted according to the previously determined frequential content, the strategy enabling at least one applicable control law to be identified. | 07-14-2011 |
20110299062 | DEVICE AND METHOD FOR DETECTING AND MEASURING WIND FOR AN AIRCRAFT - The invention relates to a device for detecting and measuring wind at the front of an aircraft, said device comprising a lidar for the cyclic measurement of wind speeds at least a couple of measuring points located at the same distance, so-called measuring distance, from the nose of the aircraft. The invention is characterised in that it is suitable for measuring wind speeds, at each cycle, by means of the lidar, at a plurality of couples of measuring points ( | 12-08-2011 |
20120303186 | Method And System For Aiding The Piloting Of An Airplane During An Approach - The system ( | 11-29-2012 |