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WO/2006/116089A1 |
A method and a system is provided for displaying an unusual attitude of an aircraft in a head-up display system. The system comprises an LCD projection unit (14) configured to project the unusual attitude of the aircraft and a processor ...
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WO/2006/113105A1 |
An improved system and method are disclosed for facilitatin g target aiming and aircraft control by flight crews using electronic displays. For example, an aircraft display system is disclosed that includes a database for storing target ...
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WO/2006/106211A1 |
The invention relates to a system comprising a display device displaying, on a cockpit pilot display unit (7), a set of indications (10) containing an aeroplane symbol (8) which illustrates the position of the aeroplane and a map part (9...
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WO/2006/106206A1 |
The invention concerns a device (1) comprising means (7) for searching for elements of the airport which are displayed on a display field of a screen (9), means (10) for verifying, for each of said elements, whether it forms part of a fi...
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WO/2006/104552A1 |
A relative navigation system including a first unit responsive to the motion of a first position, a second unit responsive to the motion of a second position and a processing unit that generates a relative navigation solution as a functi...
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WO/2006/091228A2 |
An embedded digitization system (100) enables a military platform to receive, transmit and process a variety of types of information for a variety of purposes. An apparatus and method provides a means to ensure information interoperabili...
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WO/2006/087276A1 |
The invention concerns the device, on board an aircraft, of data received or exchanged without any audio communication with the ground or with other aircraft by means of a data management device provided with display means showing, in a ...
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WO/2006/087709A1 |
There is provided a personal navigation system, including a head-mounted orientatio sensor, a coordinate position sensor, a head-mounted display, and a processor receiving a input from the head-mounted orientation sensor and an input fro...
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WO/2006/083408A1 |
An E-field sensing system (16, 18, 26, 28) is provided to detect the presence of obstacles (14), including wires, power lines or trip wires, as well as towers, guy wires, buildings and elevated terrain, in which a variation or tilt of th...
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WO/2006/078322A2 |
The present invention describes a drive system for an aircraft involving one or more nose wheel motors. Data regarding the nose wheel rotation is used to control the ground travel of the aircraft, to predict potential problems, to provid...
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WO/2006/074081A2 |
Disclosed is a programmable computing and display device (14) for upgrading a cockpit instrument panel (12) of an aircraft (8). The programmable computing and display device includes a plurality of processing units; a network backbone (5...
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WO/2006/073669A2 |
An improved avionics display unit (36) graphically presents meteorological phenomena data to a pilot enroute utilizing conventional pilot report (PIREP) information which includes meteorological phenomena data including phenomena locatio...
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WO/2006/068962A2 |
A system and method for operating an aircraft such that any hostile persons taking over the cockpit, for instance, terrorists or a disgruntled pilot, cannot control the flight path of the aircraft to enter restricted airspace, such as 'n...
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WO/2006/065782A1 |
Systems and methods for automatically switching to a track view mode on a vertical view display. The system determines aircraft position relative to a leg of a flight plan and switches display mode for a navigation vertical display to tr...
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WO/2006/061072A1 |
The inventive timepiece, in particular a wristwatch (1) is used in the form of a navigation aid for pilots and navigators and is characterised in that it comprises at least two concentric bezels (38, 46) one of which (46) is at least rot...
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WO/2006/048674A1 |
The invention provides methods for validating a position of an airborne platform, by comparing rate of change of a measure of barometric altitude with rate of change of a measure of geometric altitude. When the difference in rates of cha...
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WO/2006/046271A2 |
An electronic control unit includes in combination: data collection means form sensors and instruments existing on board of the transport means, collected-data processing means, data storage means, graphic display means, radio communicat...
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WO/2006/040441A1 |
The invention relates to an avoidance method and system for an aircraft, said avoidance system (1) comprising an anti-collision system (3), calculation means (4) for automatic determination of avoidance instructions, on an alarm, from av...
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WO/2006/040249A1 |
The invention concerns a method for a navigational aid method for an aircraft including a step of positioning an execution order in a flight plan then in a flight path. When the execution of the order is delayed, that is the order includ...
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WO/2006/032549A2 |
The invention concerns the signalling, to a pilot of a moving craft, for example an aircraft, of lateral maneuver margins taking into account obstacles placed in the maneuvering zone. Said device determines the maneuvering zone of the ve...
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WO/2006/029935A1 |
The invention relates to a device for warning the driver of a moving object about risks which are created by obstacles in the area of movement thereof. The inventive device determines the outlines of several hazardous regions (33, 34, 35...
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WO/2006/024746A1 |
The invention relates to an aircraft display system (1A). The inventive system consists of: a display device (2) comprising information sources (3) which contain information relating to the aircraft and the surrounding environment; infor...
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WO/2006/025860A2 |
Systems and methods for handling incoming aircraft operation instructions are disclosed. A method in accordance with one embodiment of the invention includes receiving from a source off-board an aircraft an instruction for changing a cha...
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WO/2006/024744A1 |
The invention concerns a device comprising a set of data sources, a data processing unit, and a display which presents on a display unit (8) attitude control indicators (9, 10, 11) representing at least speed, altitude and attitude data ...
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WO/2006/021815A1 |
A navigation display system for a vehicle comprising processing means for storing a route plan, the route plan having a predetermined position and time at each point along its length, means for displaying the route plan, means for determ...
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WO/2006/019417A1 |
A method for displaying attitude, heading, and navigation data on a single display (140) is described. The method comprises configuring the display with terrain (142) data, overlaying the terrain display with a compass rose (148) display...
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WO/2006/019420A2 |
Methods and systems for displaying aircraft operations information are disclosed. A method in accordance with one embodiment includes receiving operations information, presenting a first portion of the information over a first area of a ...
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WO/2005/123443A2 |
The invention relates to a method of indicating the lateral manoeuvre margins on either side of the flight plan path of an aircraft. The parts of the flight plan of an aircraft corresponding to low-altitude lateral paths can comprise pas...
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WO/2005/124279A1 |
The parts of the flight plan of an aircraft corresponding to lateral paths at low altitude can contain passages limiting lateral manoeuvring liberty either by risks of terrain collision or of penetration into flight prohibited area. The ...
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WO/2005/120902A1 |
An automotive display device, which allows the user to easily recognize the sameness of an information image even if the shape of the image is changed, is realized. An automotive display device (1) includes a display section (13) for dis...
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WO/2005/108924A1 |
The present invention includes an artificial horizon device including a sensor unit with a movable platform, at least one actuator linked to the platform, and one or more sensors located on the platform for sensing the position orientati...
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WO/2005/109807A1 |
The invention relates to a method for serially transmitting data between a transmitter (10) and a receiver (11), wherein said data is expressed by means of predefined words (21, 22, 23) comprising consecutive bits each of which is in a l...
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WO/2005/098367A1 |
The invention relates to a display device which is used to display a 2D topographic map corresponding to terrain sections having an essentially-horizontal profile (71, 72, 73, 81, 82, 83), said sections being referenced in relation to an...
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WO/2005/093374A1 |
The invention relates to optoelectronic taxi-assistance devices for aircraft, comprising a head-up display which can be used to display information in the pilot's field of vision. The invention is suitable for large civil aircraft of the...
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WO/2005/086114A1 |
A method for enhancing ground situational awareness to an aircraft (102) operating at an airport is described. The method includes displaying, within the aircraft, runways (104) and taxiways (122) for the airport and displaying a positio...
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WO/2005/084021A2 |
Methods and apparatus are provided for displaying data categories each having a plurality of data subcategories. The apparatus comprises a display having a current luminous output capacity that is configured to produce a first visual pre...
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WO/2005/079197A2 |
A graphical display of a vertical speed indicator showing “fly-to” and “no-fly” commands on the periphery of a vertical speed indicator during TCAS traffic or resolution advisory conditions.
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WO/2005/064277A1 |
Methods and apparatus are provided for interactively building flight paths for entry into an aircraft flight management system (FMS). The apparatus comprises a database containing map information, a display for presenting the map informa...
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WO/2005/061994A1 |
Methods, systems, and computer program products for re-sampling terrain data in a vehicle from latitude/longitude format into a Cartesian format. The present invention permits incremental updates of the terrain elevation map as the vehic...
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WO/2005/057132A1 |
A navigation system with resume logic and mode logic provides as an output an accurate navigation solution using multiple RF sensors. The resume logic determines which sensors are currently providing good data to the navigation system. T...
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WO/2005/057133A1 |
A display system and method for an aircraft simultaneoulsy displays the terrain under the flight plan, or under the current track of the aircraft, as both a two-dimensional lateral situation view image (206) and as a perspective vertical...
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WO/2005/045785A1 |
The invention relates to a system for air traffic management ATM with co-operating aircrafts that are provided with a flight management calculator FMS, are connected to the control authority via a data transmission system ATN, and have p...
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WO/2005/044650A1 |
The invention relates to a device for determining the centre of rotation of a vehicle about a vehicle vertical axis. Said device determines the centre of rotation in accordance with a yaw rate and an attitude angle.
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WO/2005/038748A2 |
A system and method is provided for transmitting, receiving, initiating, and displaying textual air traffic control clearance messages simultaneously with a graphic representation of an aircraft flight plan. Data representative of a curr...
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WO/2005/034368A2 |
A graphical display of a nonlinear scale emulating the view of a mechanical drum gauge. The nonlinear scale may be used for the display of aircraft flight data including airspeed, altitude, heading, and other aircraft data suitable for p...
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WO/2005/033631A1 |
A new method and a device is suggested. It contributes to solve air traffic congestions, improve safety, and reduce faults to simplify cockpit equipment. The method serves for the navigation of airplanes from port to port with the help o...
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WO/2005/028998A2 |
A graphical display or presentation of lateral ANP/RNP information for RNAV environments. The display may also be adapted to present aircraft data for monitoring the vertical flight performance of an aircraft under RVSM.
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WO/2005/026771A2 |
A ring cavity laser has at least two facets and a mechanism is provided to produce unidirectional propagation and light emission at a first wavelength. A source of laser light at a second wavelength is injected into the cavity to reverse...
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WO/2005/013204A2 |
A flight situation presentation system (100) displays a large majority of the information required for piloting an aircraft in an enhanced manner to reduce potential for misinterpretation and instances of piloting error. Approaches inclu...
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WO/2005/012838A2 |
Methods and apparatus are provided for generating an integrated vertical situation display. The method comprises generating a profile view frame, producing a first profile view of a first track of the vehicle in the profile view frame be...
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