Matches 1 - 17 out of 17


Match Document Document Title
US20110187562 Method And Device For Preventing An Anti-Collision System On Board An Airplane From Emitting Alarms, During An Altitude Capture Maneuver  
According to the invention, the device (1) comprises means (4) for adapting the altitude capture maneuver, means (5) for first detecting the emission of a first type alarm, means (6) for...
US20110270473 SYSTEMS AND METHODS FOR PROVIDING A VERTICAL PROFILE FOR AN IN-TRAIL PROCEDURE  
A vertical profile for an in-trail procedure can provide a pilot with enhanced situational awareness. Such a vertical profile may be able to provide a graphical indication of a clearance window...
US20140074324 METHODS AND SYSTEMS FOR INDICATING WHETHER AN AIRCRAFT IS WITHIN DISTANCE AND ALTITUDE CRITERIA FOR AN IFR PROCEDURE TURN  
Methods and systems are provided for displaying visually distinguishing characteristics if an aircraft is below a minimum altitude or beyond a maximum distance when executing a procedure turn. A...
US20140354455 SYSTEM AND METHOD FOR INCREASING SITUATIONAL AWARENESS BY DISPLAYING ALTITUDE FILTER LIMIT LINES ON A VERTICAL SITUATION DISPLAY  
A system and method are provided for increasing vertical situational awareness when the display of intruder aircraft on a vertical situation display (VSD) is restricted to a specific region of the...
US20110169665 AIRCRAFT NAVIGATION ACCURACY DISPLAY SYSTEM  
An aircraft display system is provided for rendering at least aircraft estimated position uncertainty (EPU) and/or vertical estimated position uncertainty (VEPU) values non-numerically and in a...
US20120056760 Method And Device For Automatically Determining An Erroneous Height Value Of A Radioaltimeter Mounted On An Aircraft  
Method and device for automatically determining an erroneous height value of a radio altimeter mounted on an aircraft. The device (1) includes means (12, 13, 15) for comparing the duration between...
US20100090867 Method and System for Meteorological Monitoring Aboard an Aircraft  
A method and system for meteorological monitoring aboard an aircraft. According to the invention: the altitude difference between the current altitude of the aircraft and the altitude of the...
US20070176794 Synthetic Vision Final Approach Terrain Fading  
A method of removing synthetic vision terrain and objects from a graphical display when unsafe to rely on the synthetic vision terrain and objects is provided. The method comprises receiving...
US20090109064 Simplified self-powered attitude survival indicator  
This simplified self powered aircraft attitude survival indicator is easily and readily transportable from one aircraft to another and provides a simple indicator which gives a visual indication...
US20100033350 STANDBY INSTRUMENT FOR AN AIRCRAFT INSTRUMENT PANEL DETECTING OVERLOAD, PARTICULARLY DURING THE LANDING PHASE  
The present invention relates to a standby instrument fitted to the instrument panel of an aircraft detecting overloads. The standby instrument includes a processor to calculate and display flight...
US20090189787 SYSTEM AND METHOD FOR GENERATING AN ALTIMETER MIS-SET ALERT ON A PRIMARY FLIGHT DISPLAY  
A primary flight display system is provided for deployment on an aircraft including a barometric altimeter and a secondary altitude-determining device. The barometric altimeter provides a first...
US20120001773 AVIONICS DEVICE, SYSTEMS AND METHODS OF DISPLAY  
The present general inventive concept relates to methods and systems to select and display information on an avionics display screen. The systems and methods allow for the selection and display of...
US20070247350 Method and apparatus of compressing terrain data  
A method and apparatus for reformatting terrain data that in turn increases compressibility of the terrain data. The method includes storing each sample of terrain data as a signed integer offset...
US20110273315 SYSTEMS AND METHODS FOR ADJUSTING LANDING GEAR ALERT ENVELOPE FOR OFFSHORE PLATFORMS AND BUILDING-TOP LANDINGS  
Systems and methods for improving landing gear alerting on a rotary wing aircraft. An example system includes a user interface device that allows a user to set a bug altitude value and a radio...
US20130106623 SYSTEMS AND METHODS FOR ADJUSTING SINK RATE ALERT ENVELOPE FOR SPECIAL LANDING ZONES  
Systems and methods for improving sink rate alerting for rotary wing aircraft. In one example, the system includes a radio altimeter that produces an altitude value, a processor that is in signal...
US20100141481 Multi-stage label  
An aspect of the present invention provides a method for providing information to an air traffic controller. The method comprises the steps of: displaying, on a video display, a symbol...
US20110199237 METHODS AND SYSTEMS FOR DEPICTING A DATA DRIVEN MINIMUM SAFE ALTITUDE  
A method for providing a minimum safe altitude indication on an aircraft display is described. The method includes utilizing current aircraft heading and position data to generate a location and...

Matches 1 - 17 out of 17