Patent application number | Description | Published |
20100128251 | METHOD AND DEVICE FOR DETERMINING ANEMOMETRIC PARAMETERS OF AN AIRCRAFT - A method and device for determining anemometric parameters of an aircraft. | 05-27-2010 |
20100128252 | METHOD AND DEVICE FOR OPTIMIZING THE ORIENTATION OF A LASER ANEMOMETER ON AN AIRCRAFT - The device ( | 05-27-2010 |
20100131230 | METHOD AND SYSTEM FOR MONITORING PARAMETERS OF AN AIRCRAFT - According to the invention, the monitoring system comprises two laser anemometers and a selection logic device able to select, on the one hand, a value of the IAS air speed to be displayed on first display means and, on the other hand, another value of the IAS air speed to be displayed on second display means. | 05-27-2010 |
20110253840 | METHOD FOR INSTALLING AN INERTIAL REFERENCE UNIT IN AN AIRCRAFT, AND AIRCRAFT EQUIPPED IN THIS WAY - The invention relates to a method for installing an inertial reference unit in an aircraft, in which: a reference unit support ( | 10-20-2011 |
20110264308 | Method And Device For Automatically Estimating An Air Speed Of An Aircraft - The device ( | 10-27-2011 |
20120092193 | Method And Device For Aiding The Managing Of Air Operations With Required Navigation And Guidance Performance - The device ( | 04-19-2012 |
20120150367 | Method And Device For Automatically Monitoring The Ability Of An Aircraft To Follow A Flight Trajectory With At Least One Turn - Method and device for automatically monitoring the ability of an aircraft to follow a flight trajectory with at least one turn. | 06-14-2012 |
20140136091 | METHOD AND DEVICE FOR ENSURING THE ACCURACY AND THE INTEGRITY OF AN AIRCRAFT POSITION ON THE GROUND - An assist device for ensuring the accuracy and integrity of position information of an aircraft on the ground includes means for determining in the airport (AE) a zone (ZP) of insensitivity to multipath GPS signals, the zone (ZP) having a rectangular shape, which is determined relative to the threshold (O) of the runway, and which has a length (L | 05-15-2014 |
20150081144 | METHOD AND A DEVICE FOR AIDING PILOTING OF AN AIRCRAFT DURING AN APPROACH PHASE FOR LANDING - A method and device for aiding piloting of an aircraft during an approach phase for the purpose of landing. The device includes a guidance system for guiding the aircraft according to a first guidance mode during an initial phase upstream of a transition point, then guiding the aircraft according to a second guidance mode during a terminal phase between the transition point and the landing, the device further including a computing system for automatically computing the coordinates of the transition point, the guidance system also configured for automatically disabling the second guidance mode upstream of the transition point. | 03-19-2015 |
20150219460 | DEVICE AND METHOD FOR PREDICTION ON THE GROUND OF CHARACTERISTICS OF THE POSITION OF AN AIRCRAFT ALONG A PATH - A prediction device for prediction on the ground of characteristics of the position of an aircraft along a path is provided. The prediction device comprises a calculation element comprising a performance and integrity model consistent with a model on board an aircraft. The second calculation element determines precision, integrity and availability information concerning the position of the aircraft along a flight and/or ground path. The integrity information taking account of an integrity of a satellite positioning system and at least one hardware integrity on board the aircraft. | 08-06-2015 |
20160026178 | METHOD AND DEVICE FOR AUTOMATICALLY MANAGING AIR OPERATIONS REQUIRING A GUARANTEE OF NAVIGATION AND GUIDANCE PERFORMANCE OF AN AIRCRAFT - Method and device for automatically managing air operations requiring a guarantee of navigation and guidance performance of an aircraft. The device for automatically managing at least one air operation comprises activatable monitoring of the air operation, a computation unit configured to automatically calculate an anticipated activation point as a function of the application point of the air operation, this anticipated activation point being defined upstream of the application point in the direction of flight of the aircraft, and an activation unit configured to automatically activate monitoring and a display when the aircraft reaches, during its flight, the anticipated activation point. | 01-28-2016 |