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WO/1998/022923A1 |
In a terminal co-ordination system, the data required for the flight safety personnel to carry out their control activities, taking into account the flight schedule data for handling actual arrivals, departures and crossings, as well as ...
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WO/1998/015912A1 |
A navigation system includes a processor (20) and bit-mapped earth surface map image data in a first data storage device (28) accessed by the processor (20), the processor (20) displaying an image essentially filling a display area of a ...
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WO/1998/012687A1 |
A device is described for simulating in real time the position of a possibly fictitious object in a three-dimensional coordinate system, comprising at least a first unit and a second unit. Each unit is provided with a GPS-receiver (2) fo...
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WO/1998/012685A1 |
A system for the remote activation and operation of access control or reading of navigational guidance equipment located at a distant facility such as an aerodrome or harbour by means of radio. The invention allows the operator of a vess...
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WO/1998/010398A1 |
Man-Machine Interface (MMI) for aiport traffic control, especially for safe traffic management and/or landing and take-off control at an airport, comprising a display surface on which procedures and states at the airport are indicated an...
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WO/1998/010308A1 |
The invention concerns a method of air navigation or steering assistance for guiding a moving vehicle towards a target whose exact position is not known a priori, in particular a moving target. It is suggested that the moving vehicle and...
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WO/1998/004929A1 |
A fail safe GPS system for an aircraft moving along a desired trajectory within vertical and horizontal limits using first and second redundant GPS receivers a first of which is connected to the avionics equipment of the aircraft and to ...
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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/1998/003881A1 |
A differential ground station repeater in which a plurality of transmitters are utilized to relay information to an aircraft from a single ground station situated to receive satellite information and to transmit the satellite and other i...
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WO/1997/047947A1 |
For the lateral avoidance of a fixed zone (10), the method comprises successively: modelling the contour of the zone to be avoided (10) by a convex polygonal form (11), locating the scheduled route (2) with respect to the modelled zone (...
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WO/1997/047946A1 |
For controlling a vehicle in order to change course, the vehicle (1) following a first rectilinear route portion (R1), to join a second rectilinear route portion (R2) forming a predetermined angle () with the first route portion (R1), pa...
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WO/1997/047945A1 |
For the lateral avoidance of a mobile zone (10) by a vehicle (1) based on periodically supplied information concerning the mobile zone to be avoided (10) and on an initially scheduled route (2) for the vehicle, the method comprises: defi...
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WO/1997/041450A1 |
This invention is directed to a method and apparatus to track a target and enable high data transfer rates between the target, such as an aircraft, and a base station by electromagnetic radiation means. The position of the aircraft is ca...
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WO/1997/041495A1 |
The invention relates to air navigation assistance methods and devices, used in flight management systems on board aircraft. To facilitate the work of the pilot, the onboard computer (FMS) communicates with the pilot through a display an...
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WO/1997/040401A1 |
A hazard alert device for aircraft prioritizes various alerts according to predefined criteria. The device enables more optional alerting of hazardous conditions than a system of separate independent and discrete devices.
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WO/1997/037336A1 |
An object detection system including passive sensors (3) for receiving electromagnetic radiation from a moving object (28) and generating intensity signals representative of the received radiation, and a processing system for subtracting...
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WO/1997/034276A1 |
In a method of detecting a collision risk and preventing air collisions, it is proposed that probabilities should be calculated for the likely presence of one's own aircraft in predetermined sectors at a number of selected times (probabi...
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WO/1997/032291A1 |
The invention relates to an airport surface movement guidance and control system (SMGCS) involving detection, integrated processing and graphic representation of the relevant, in particular with respect to safety, positions and movements...
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WO/1997/026552A2 |
This invention proposes equipping aircraft (10, 12, 14) and other objects with a monitoring unit (16, 18, 20) in order to monitor the path of such objects independently of a control center. The monitoring unit continuously emits the posi...
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WO/1997/026637A1 |
The invention relates to air navigation aid devices and methods used in flight management systems onboard of aerodynes. In order to facilitate the task of the pilot, the onboard computer (FMS) dialogues with the pilot through a multipurp...
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WO/1997/026553A1 |
An aircraft piloting aid system mainly used during take-off and landing under adverse visibility conditions is disclosed. To make use of head-up displays which display artificial horizon line, aircraft pitch attitude and ground speed vec...
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WO/1997/019432A2 |
A system to alter the voltage supplied to the linear regulator of a pulsed transmitter in accordance with the temperature of the regulator, the minimum voltage required for a transmission and the specific aircraft installation requiremen...
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WO/1997/014114A1 |
An aircraft docking system (46) within a dock in full view of an approaching aircraft (20) and in view of the pilot, has a display which is readily seen by the pilot as the aircraft proceeds along a taxiway and during a turning of the ai...
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WO/1997/011421A1 |
A method for interactively displaying flight information in an air traffic control system. Flight information lists (40, 60, 90) are displayed relative to associated geographic fixes (201, 301, 401), and further flight information is dis...
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WO/1997/011421A2 |
A method for interactively displaying flight information in an air traffic control system. Flight information lists (40, 60, 90) are displayed relative to associated geographic fixes (201, 301, 401), and further flight information is dis...
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WO/1997/006500A1 |
A horizontal miss distance filter system (220) is provided for inhibiting resolution alert messages from an air traffic alert and collision avoidance system (210) to a pilot's display (230). The horizontal miss distance filter employs a ...
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WO/1997/004337A1 |
A device for detecting the presence or absence of an object, its movement, moving direction, speed, shape, quantity and their time information without being provided with transmission means. An antenna device (1) has the function capable...
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WO/1996/038831A1 |
A system for enhancing navigation or surveillance in low visibility conditions is realized by employing one or more ultraviolet radiation sources (110), a receiver (130) which is capable of producing output signals from which a two dimen...
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WO/1996/020465A1 |
The invention is related to a method for surveying zones wherein, primarily, aeroplanes move, a scanner (A), preferably of the laser radar type, being caused to deliver information to an automatical control or docking system. This occurs...
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WO/1996/012265A1 |
A system for detecting, identifying and docking aircraft using laser pulses to obtain a profile of an object in the distance. The system initially scans the area in front of the gate until it locates and identifies an object. Once the id...
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WO/1996/005562A1 |
This invention provides a method and apparatus to provide coordinated evasive maneuver commands to aircraft to avoid collision. More specifically, the invention comprises a gps system to determine the location of aircraft, control logic ...
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WO/1996/002905A1 |
A satellite based air traffic control (ATC) system includes an aircraft unit (18) on an aircraft and an ATC facility (48). The aircraft unit (18) includes an AARTS processor (28), GPS receivers (20, 22), a comparator (24) for comparing t...
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WO/1995/033213A1 |
An aircraft including an approach and landing system, including a navigation unit (2, 4, 6) for providing navigation information, a weather radar unit (8) for providing radar information, a processor (16) which receives navigation inform...
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WO/1995/031799A1 |
A user interface device for airport operation-card management system which supports the control jobs of controllers (FD, CD, GC, and LC) who perform the assigned control jobs to manage the operation of an airport in cooperation with each...
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WO/1995/028650A1 |
An aircraft location and identification system, including a firstposition determining portion (120) located aboard a transmitting aircraft for determining a first set of present positional and tracking information is described relative t...
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WO/1995/027909A1 |
The invention concerns a satellite navigation process, in particular for an automatic landing process for aircraft, according to the ICAO requirements under the CAT-II or CAT-III terms. The necessary degrees of accuracy are achieved by a...
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WO/1995/027910A1 |
An airport noise monitoring system is disclosed comprising a pair of sound detectors (200, 300) installed in and spaced along a runway. A CPU monitors the output of each sound detector so as to recognize an output form from one (200) of ...
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WO/1995/025966A1 |
A method for automatically providing weather advisories for an airport to pilots comprises monitoring weather conditions at the airport and then generating weather advisories in response to these weather conditions. The broadcast traffic...
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WO/1995/023734A1 |
The invention concerns a device for guiding the pilot of an aircraft approaching its specified parking position when it is running straight. The device comprises a distance measuring arrangement, which faces in the direction of travel fr...
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WO/1995/021388A1 |
An air traffic surveillance and communication system for air traffic controllers, includes a plurality of ground based first digital radio transceivers located in specific geographic sectors, respectively, and having a first frequency ch...
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WO/1995/019547A1 |
A computer-based process for rapidly responding to previously unknown threats to airborne aircraft. The process makes quick, automatic decisions when required for close-range threats, yet provides the aircraft operator an opportunity to ...
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WO/1995/019609A1 |
A terrain profile for executing terrain following flight is generated using a minimal volume of digital terrain elevation data (DTED) information. By limiting the amount of information considered in generating the terrain profile, the co...
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WO/1995/019544A1 |
A device executing intervisibility calculation includes a mechanism executing a radial spoke scan pattern where individual radials are traversed beginning at a threat installation and extending outward along a radial to a distance corres...
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WO/1995/019611A1 |
A convergence model is shown and described for accommodating variation in data post spacing in a digital terrain elevation database (DTED) based on longitude and latitude address values for data posts. Under such a database structure, da...
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WO/1995/019545A1 |
A method for calculating intervisibility data in advance of its use for permitting a real time update of threat information. Threat intervisibility data corresponding to an area comprised of adjacent regions is calculated and stored. A r...
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WO/1995/019543A1 |
A covert flight data processor is shown including a collection of integrated flight processing hardware and procedures. The processor devices are interconnected by a corresponding collection of bus structures providing appropriate and di...
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WO/1995/017685A1 |
A vehicle location system and method (18, 36) whereby the position coordinates of a vehicle (10) are made available to other vehicles (12) or to fixed locations (72, 74, 76) by transmission of a data message (50) containing position coor...
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WO/1995/008778A1 |
A system for measuring the relative positions of first and second units (1, 2) includes a re-transmitting apparatus at the first unit (1) and a receiver at the second unit (2) capable of making simultaneous real-time comparisons of phase...
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WO/1995/008779A1 |
A GPS system that includes a GPS beacon (26) that receives a plurality of GPS signals (25), each having a carrier component and a pseudo-random code component, and generates in response thereto a plurality of beacon signals (27) having a...
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WO/1995/003213A1 |
There is disclosed a method for operating aircraft, in which two aircraft (11) are controlled by a common control arrangement (12) to fly parallel courses within a common ATC slot.
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