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WO/2002/080128A1 |
The present invention is directed to novel methods for depicting glide range (16, 34) on moving map displays (3) and on perspective-view primary flight displays. These methods involve processing data gathered from various aircraft sensor...
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WO/2002/068905A2 |
A system for graphically displaying on a cockpit display an indication of closure (i.e. a 'closure indicator') with a selected target aircraft. In a preferred embodiment of the invention, the system only displays a closure indicator if: ...
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WO2002040943A9 |
The present invention disclosure is related to various systems and methods designed to simplify the use of flight management systems on an aircraft. The present invention provides a method and system for displaying a flight plan such tha...
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WO/2002/058033A2 |
A system and method for filtering various targets (such as ground vehicles, stationary objects, and aircrafts) from displays on a display screen within the cockpit of an 'Own Ship' aircraft. The system and method withhold from display an...
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WO2000065423A9 |
The present invention is directed to novel primary flight displays (3), moving map displays (8, 9) and engine parameter displays (15, 16, 17) for aircraft cockpits. These displays process data gathered from various aircraft sensors and, ...
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WO/2002/046699A1 |
A vehicle navigation system combining inertial, altitude and gps measurements with the corresponding interfaces and sharing the position and orientation information with other flight instrumentation via data bus.
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WO/2002/045048A1 |
The invention concerns a landing system enabling navigation and landing by supplying a virtual image of the immediate surroundings, obstacles, other vehicles, ground navigating stations (VOR, NDB, and the like), standard reporting points...
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WO/2002/039058A2 |
Methods and apparatus are provided for airspace navigation. Airspace navigation information for an aircraft is displayed in a first mode, such as, in a horizontal mode. One or more navigation events may then be detected, such as, proximi...
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WO/2002/039060A2 |
The present invention includes a system, method and computer program product for reducing nuisance warnings during low performance takeoff conditions. The system includes a first component that determines aircraft current clinb rate and ...
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WO/2002/039407A1 |
Anti-collision device that uses only the GPS coordinates avoiding any radio-navigation system. A processor creates an imaginary line ideally projected ahead the bow of the aircraft, which meets the obstacles coming across the course. Thi...
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WO/2002/031795A2 |
The present invention provides systems and methods (100) for an integrated graphical user interface (114) which facilitates the display and editing of non-flight plan information (304). In accordance with various aspects of the present i...
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WO/2002/031796A2 |
A method of simultaneously presenting a textual display of an original flight plan and a modified flight plan includes displaying a texlist of waypoints, copying waypoints from the original flight plan into the modified flight plan, comp...
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WO/2002/029363A2 |
A navigational system includes a display device and logic that simultaneously presents a textual display of an original flight plan and a modified flight plan on the display device. The textual display includes a textlist of waypoints th...
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WO/2002/029362A2 |
The pilot's awareness of the aircraft's state is enhanced by supplementing the flight modes area (FMA) 30 in the upper region of the primary flight display (PFD) 5 with additional annunciators. The FMA 30 in the present invention display...
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WO/2002/025215A2 |
The completion of an electronic checklist is facilitated by the automated display of certain data while completing the checklist. The disclosed program presents an automated display of synoptic, navigational, or flight management data fo...
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WO/2002/025213A2 |
A system, method and device for selecting and displaying navigational information is presented which includes a display for showing navigational procedures and/or options, means for selecting or deselecting the procedures and/or options,...
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WO/2002/025208A2 |
The pilot or crew of an aircraft is alerted to the danger presented by wires in the vicinity of the aircraft by a flight instrument which includes a plurality of wire detected display elements (40, 41, 42), advantageously arranged as bar...
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WO/2002/024530A2 |
An aircraft display and control system (100) generally includes a processor (106), a cursor control and selection device (104), a multifunction keyboard (116), an aeronautical information database (110), a geographic database (108), and ...
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WO/2002/025214A2 |
Various embodiments of the invention suitably provide dialog boxes (400, 500, 600, 700, 800, 900) in response to pilot commands so that task parameters may be input or modified. Pilot tasks include 'direct-to', 'hold', 'procedure turn', ...
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WO/2002/025211A2 |
An aircraft display and control system (100) generally includes a processor (106), a cursor control and selection device (104), an aeronautical information database (110), a geographic database (108), and a plurality of display devices (...
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WO/2002/025618A2 |
A system and method for graphically controlling a communication device and displaying its characteristics on a display within a vehicle including a microprocessor, a communication and navigation information window within a portion of the...
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WO/2002/007094A2 |
The present invention includes a display for viewing information, where a number of lines on the display has a variable line resolution scale. Each of the number of lines corresponds to a value of information, such as angle degrees relat...
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WO/2001/096812A2 |
A method and apparatus for displaying real time navigational information on a vehicle including an informational database which is loaded and stored on an electronic medium within the vehicle. An intermediate database is created from the...
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WO/2001/094890A2 |
An embedded digitization system (100) which enables a military platform to receive, transmit and process a variety of types of information for a variety of purposes. The system includes a mission processing capability (110, 420), a digit...
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WO/2001/053148A1 |
The invention concerns a device (10) for measuring one or several navigation parameters in a large-size navigating craft, comprising a parameter sensing and measuring element (11) and at least means for displaying (12) said parameter, co...
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WO2001006476A9 |
A human centered informational display system (named OZ) is disclosed that can be used with vehicles (e.g. aircraft) and in other operational environments where rapid human centered comprehension of an operational environment is required...
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WO/2001/025727A1 |
A system (100) for producing vehicle routes such as aircraft flight plans (120, 410) in the presence of weather and other hazards (120, 420) defines static and moving hazards with polygons (220, 230, 430) drawn on a display (152, 400) co...
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WO/2001/020583A2 |
A flight information display for the flight deck of an aircraft showing a pictorial side view of the flight path or the area directly in front of the aircraft area having a selected distance of at least 0.5 nautical miles, comprising (a)...
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WO/2001/020261A1 |
The invention concerns the navigation of aircraft (planes and helicopters) and can be used in favorable or complicated weather conditions, during the takeoff roll, takeoff, descent and approach. The system, which ensures the automatic co...
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WO/2000/071985A1 |
A circuit and method for predicting an intersection of a host aircraft flight path with the wake vortex of another aircraft.
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WO/2000/057202A2 |
The ground proximity warning system and method provide a number of alerts based upon a substantially reduced list of input parameters relative to a conventional ground proximity warning system and method. The ground proximity warning sys...
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WO2000016230A9 |
A computer system (10) for displaying on a display device (30) terrain, weather and aviation information and including memory devices (16, 18, 20) which contain a terrain database, aviation map database, weather database, air traffic dat...
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WO/2000/041000A1 |
A passive Traffic Alert and Collision Avoidance System (TCAS) and method is based on receiving and processing Mode-S transponder messages without the TCAS computer having to interrogate the transponders of the respective aircraft flying ...
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WO/2000/022382A1 |
The invention concerns standby instruments to assist piloting of an aircraft designed to supply, with high operating safety, indications concerning the aircraft pressure altitude, calibrated airspeed and attitude (roll and pitch angles),...
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WO1999057511A9 |
In order to improve the representation of the terrain on a Primary Flight Display and a navigation display, the terrain is represented at least partially in the form of a stratified model of the terrain and/or the representation of at le...
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WO/2000/002008A1 |
Improved multifunction probe having circumferentially separated pairs of sensing ports (22, 24).
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WO/1999/058358A1 |
The invention relates to a driver assistance system of a motor vehicle and to a method for operating a drive assistance system of a motor vehicle. The invention comprises a detection means (24, 28, 30) for predetermined, instantaneous en...
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WO1999032850A9 |
In order to provide the pilots with a display or a map of the terrain below the aircraft, a display is generated on a cockpit display, such as a weather radar, of the contours of the terrain below the aircraft. The terrain contour displa...
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WO/1999/022960A1 |
An instrument panel (10) having easy-to-read instruments is disclosed and which in certain embodiments allows for more efficient use of space behind the instrument panel (10) by providing a partially reflective screen (16) in the instrum...
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WO/1999/022206A1 |
Taxi and slope landing symbology for a helicopter having a main rotor drive shaft and a main rotor hub defining a hub moment, wherein the main rotor drive shaft and the main rotor hub have hub moment limits. The taxi and slope landing sy...
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WO/1999/003000A1 |
An improved navigation and display system especially suitable for small aircraft rapidly determines the attitude (roll and pitch) of an aircraft from measurements made by an inexpensive, single receiver and antenna responsive to signals ...
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WO/1998/039620A1 |
The invention relates to a flight guidance system for low-flying aircraft. A base image is provided by the natural vision of the pilot or produced by means of a sensor, this being an image of the scene in front of the aircraft. The inven...
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WO/1998/022780A1 |
An aircraft display system positions a synthetic runway which is properly aligned with a target runway even during crosswind approaches. The relative position of the target runway is computed in a manner which reduces the accumulated err...
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WO/1998/013667A1 |
An integrated aircraft control system in which the avionics functions of flight control are united with the utility functions of aircraft tending in an overall integration system utilizing a pilot cockpit display for producing control si...
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WO/1998/005928A1 |
Vehicle steering assistance, particularly for instrument landings, is disclosed. A horizon line with a heading scale, a perpendicular line with an attitude scale, an aircraft symbol (O) indicating the direction of the longitudinal axis o...
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WO/1998/005017A1 |
An embedded mission avionics data link system is provided which allows an aircraft to receive, transmit, and process a variety of different types of information. The present system has the capability of generating and receiving video inf...
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WO/1998/004883A1 |
In order to provide the pilots with a display or a map of the terrain below the aircraft, a display is generated on a cockpit display, such as a weather radar, of the contours of the terrain below the aircraft. The terrain contour displa...
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WO/1997/048969A1 |
The present invention provides a radio navigation emulating GPS device. In one embodiment, the radio navigation emulating GPS device receives an identifier associated with a conventional radio navaid. The present radio navigation emulati...
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WO/1997/043704A1 |
An improved aircraft flight management system includes a flight management computer (FMC), left and right control display units (CDU's) and a backup CDU. A triple redundant digital databus links the FMC and three CDU's. Upon detecting a ...
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WO/1997/039311A1 |
A process and system are disclosed for representing flight guiding information for an aircraft. A spatial representation of the air space with at least one horizon and the previously calculated flight path of the aircraft is represented ...
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