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WO/2003/024795 |
The invention concerns an anti-hijacking device for an aircraft in flight comprising a mechanism for cancelling and restoring flight controls of a hi-jacked aircraft while ensuring the safety flight personnel.
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WO/2003/025962 |
A standardized control panel for aircraft provides manually operable controls that are configured to activate an aircraft function if the requested aircraft function is installed on the aircraft or, are otherwise configured to activate a...
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WO/2003/025905 |
The present invention includes a processor configured to receive at least one operating parameter from an operating parameter input and, based on the operating parameter, configure at least one filter to filter a signal.
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WO/2003/023734 |
Methods and apparatus are provided for generating a vertical situational image of a vehicle. The apparatus for generating a vertical situational image of the vehicle is comprised of an input device configured to receive flight plan data ...
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WO/2003/021549 |
A vehicle detecting system and method for use on a specific location such as an airport, including a sensor string nominally perpendicular to the direction of vehicle travel at the location. The sensor string includes at least one magnet...
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WO/2003/019313 |
Disclosed are combinations of electronic navigation systems for aircraft landing approaches, enabling overall operating complexity (especially on the ground) of electronic aircraft guidance systems for precision approaches to be reduced ...
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WO/2003/009255 |
A formation collision avoidance system includes a Traffic Alert and Collision Avoidance System (TCAS) having a passive mode and an active mode. The passive mode enables several members of an aircraft formation to fly without actively int...
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WO/2003/005326 |
A system and method for displaying a three-dimensional image of airspace includes a series of translucent, horitontal 'pavers' that lie like stepping stones marking the selected flight path. In addition, the display includes a series of ...
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WO/2003/004352 |
An airship system, comprising an airship (110), a base station (120), and at least three measurement points, wherein, when the airship (110) receiving an instruction from the base station (120) transmits ultrasonic wave, the measurement ...
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WO/2003/005058 |
A computer generated pilot instruction system for providing spatial information to a pilot corresponding to the difference between the actual landing flight path and optimal landing flight path.
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WO/2003/002944 |
The invention relates to methods for the display of cartographic information on an aeroplane screen. Said method concerns the display of several windows (2D5, 3D, PV, PH) on an aircraft screen, each representing a distinct aspect of the ...
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WO/2003/002941 |
The invention relates to a method for generation of a relief image, comprising pixels and representing, in colour, the terrain over which an aircraft is flying, with at least one normal anti-collision mode in which the colour representin...
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WO/2003/002940 |
The invention concerns a method for synthesis of a chart image consisting of pixels and representing a terrain flown over by an aircraft, the chart imagery being developed in each pixel from several data including, a first colour altimet...
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WO/2002/103507 |
The invention relates to methods of managing a man/machine interface in a cartographic system that is at least partially located on-board an aircraft. Said interface links a designator and an aircraft screen and provides a connection bet...
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WO/2002/101685 |
In-flight refuelling of a fleet (1) of aircraft by a refuelling aircraft (2) through a refuelling boom requires that a queue is formed and that the number, one or possibly two, of passages for each aircraft at the refuelling boom is dete...
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WO/2002/101686 |
A navigation and guidance computer system using navigation sensors to determine aircraft position, and automatically control the aircraft to fly from an initial position (410, 502) to intercept and follow a crew-selected rendezvous orbit...
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WO/2002/099769 |
The proposed architecture for an air traffic management system concentrates on information exchange to provide trajectory-based flow and flight planning, and separation assurance. The various Control, Navigation, and Surveillance element...
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WO/2002/097570 |
Open Pairings occurring during airline operations are repaired n at a time (where n is an integer) in near real time through use of two solution paths, one involving one-way fixes, and the other matching transformations. From the resulti...
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WO/2002/095712 |
A method is presented for managing, in real time, the arrival and departure of a plurality of aircraft to and/or from a specified system resource (e.g., an airport, gate, section of airspace) or set of system resources based upon conside...
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WO/2002/095709 |
A Surface Movement Area/Runway Traffic and Surface Area Flow Tool with Runway Incursion Protection System reduces runway incursions due to lost or disoriented aircraft, navigation in low visibility conditions, unfamiliarity with local pr...
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WO/2002/091595 |
A data link is used to deliver guidance information, derived from an external system, to one or more aircraft. The guidance information is then used to form analog signals or digital messages, on board the aircraft, which emulate the out...
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WO/2002/089088 |
An aircraft (30) landing on a runway (28) and moving in a certain direction (36) is directed to exit the runway (28) on a particular exit taxiway (38). While on the runway (28), the aircraft (30) passes through a cone-shaped dispersion p...
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WO/2002/082407 |
A system is provided for managing the inbound flow of aircraft to an airfield by ensuring that aircraft are sequenced before departure into an arrival stream. Sequencing uses operational data obtained from airlines and then provides a me...
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WO/2002/071367 |
A system for alerting the occupant of a vehicle that the vehicle is in or approaching a zone of awareness. For instance, the system may be used to alert the pilot or flight crew of an aircraft (101) that the aircraft is on or approaching...
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WO/2002/068991 |
A system and method for displaying target vehicle (22, 24, 26) position combines the data available from a plurality of surveillance sensors. Data from the plurality of sensors (52, 54, 56, 58) is fused to calculate a composite target po...
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WO/2002/068905 |
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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WO/2002/067222 |
The invention concerns a system for displaying in space of a trajectory between at least a transmitter and a receiver, one or the other being mobile. Said spatial display system of a trajectory between at least a transmitter and a receiv...
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WO/2002/063589 |
An automatic detecting system for detecting occurrence of an important event for an civil airline such as TAKEOFF, LANDING, G0-AROUND, DIVERT after entry into an approach area, REJECT-TAKEOFF, arrival at an arbitrarily set altitude, entr...
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WO/2002/058032 |
An improved airplane warning sphere for day and night installed to an aerial wire, which lights illuminating elements at night by using the electricity charged by solar cells at day so that a pilot of a helicopter or airplane may easily ...
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WO/2002/058033 |
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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WO/2002/056054 |
A system for detecting, identifying and docking aircraft using laser pulses to obtain a profile of an object in the distance initially scans the area in front of the gate until it locates and identifies an object. Once the identity of th...
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WO/2002/052546 |
An interactive voice response system is described that supports full duplex data transfer to enable the playing of a voice prompt to a user of telephony system while the system listens for voice barge-in from the user. The system include...
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WO/2002/052526 |
A method receives terrain clearance measuring radio wave emitted from an airplane to input and record to a computer changes in electric field intensity level of the wave, and measures accurately point-blank passing time based on sharply-...
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WO/2002/048812 |
A system and method for determining the vertical integrity of an altitude component of an aircraft navigational signal through the use of a receiver-autonomous vertical integrity monitoring (RAVIM) algorithm. The system and methods also ...
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WO/2002/046699 |
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/2002/045048 |
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/2002/040943 |
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/2002/039407 |
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/2002/035497 |
The invention concerns the observation of security distance between aircraft flying, in line, one behind the other, in an imposed air corridor. More particularly, it concerns a method enabling an aircraft knowing its position and those o...
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WO/2002/035252 |
A civil aviation passive coherent location system and method is disclosed. A receiver subsystem receives reference transmissions from an uncontrolled transmitter. The receiver subsystem also receives scattered transmissions originating f...
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WO/2002/032764 |
Method and arrangement in the automatic landing of an aircraft (1), comprising a unit (4) arranged on the aircraft (1) and designed to form an image of a group of radiation sources (3) located next to a runway (2), and a calculation devi...
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WO/2002/033436 |
A surveillance transceiver system is provided for receiving extended squitters from Mode S transponders, translating the squitters into ADS-B state vectors in UAT format, and transmitting the ADS-B state vectors using a Universal Access ...
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WO/2002/031783 |
The invention concerns a method for managing ground assistance teams of a transport vehicle in a parking zone (19), wherein a management centre (3) determines the tasks for the respective assistance teams and provides each team with data...
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WO/2002/031795 |
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/2002/031796 |
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/2002/016870 |
A system, method, and computer program product for altering an aircraft flight crew of an inconsistency during an instrument landing system (ILS) approach to a selected runway.
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WO/2002/015153 |
The invention relates to a system for processing flight plan data in order to produce a sequence of take-offs and/or landings of aircraft and for documenting the main traffic operations and data for take-offs and/or landings of aircraft....
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WO/2002/010794 |
A second-order filter that blends accurate position information from a one source, and velocity information from another source, both suitably scaled, in a second-order complementary filter. The filter is arranged such that an internal i...
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WO/2002/010792 |
Improved methods and systems for detecting self-alerts from upload messages in a TIS system to thereby eliminate the likelihood of TIS self-alerts appearing on CDTI displays. The present invention determines whether a self-alert was pres...
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WO/2002/008934 |
A computer system for providing an integrated representation of routes in a transport system is disclosed. The computer system comprises a multiplicity of connectable stations. Data is obtained from a plurality of transport providers. Th...
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