Abstract: The invention relates to a database and a method of generating a database containing topographical information on obstacles distributed over a geographic area subdivided into cells. The method includes reading topographical data obtained from heterogeneous sources. Topographical data are generated which relate to pointlike obstacles from the information collected from the topographical data. Topographical data are generated which relate to linear obstacles from the information collected from the topographical data. The obstacle database is created. Each cell contains a link to the obstacles whose coordinates in the geographic area covered by the cell are recorded with an uncertainty value. In particular, the invention applies to the generation of a database on board an aircraft.

Abstract: A present novel and non-trivial system, module, and method for presenting runway advisory information are disclosed. A runway reference may be established using data received from a source of navigation reference data, where such data could represent runway information, runway awareness zone information, landing awareness zone information, and/or runway threshold line information. Navigation data representative of at least aircraft location and input factor data may be received from a source. Phase of flight may be determined using input factor data, and a runway advisory data set may be generated as a function of phase of flight and the positional relationship between aircraft location and the runway reference. Runway advisory data set may be representative of advisory information comprised of visual runway advisory information, aural runway advisory information, tactile advisory information, or a combination thereof.

Abstract: The invention relates to a light sign (10) for displaying an instruction and/or guidance for ground airplane traffic at an airport, comprising a casing (20) with a transparent display panel (21) for representing an instruction and/or guidance symbol (Z), and a light source arranged inside the casing (20) with at least one luminescent diode (32) for illuminating the display panel (21). A diffusion panel (22) is made for scattering and/or back-scattering incident light, wherein the light source is arranged between the display panel and the diffusion panel. The at least one luminescent diode (32) is aligned on the diffusion panel (22) so that the display panel (21) is not illuminated directly, but indirectly by back-scattering of the light emitted from the at least one luminescent diode by the diffusion panel (22).

Abstract: A target information storage unit (203) stores information regarding a group of targets (target panels) which are disposed dispersedly on a virtual race course and which each have an objective speed set therefor. An operation input reception unit (201) receives an operation input for a moving object (racing car) to be run on the course. Then, a running condition managing unit (204) manages the running condition of the moving object based on this operation input. Meanwhile, a passage determination unit (206a) sequentially determines whether or not the moving object has passed on the course by contacting the respective targets, based on the managed running condition. Further, a speed comparison unit (206b) compares the speed of the moving object at the time of the passage and the objective speed of each target. Then, an evaluation unit (206) evaluates the operation input from a user based on the determination result and comparison result.

Abstract: A system of signal emitting modules is disclosed. The modules emit light or other signals to warn oncoming traffic that a road or other pathway has changed or is traversing a tortuous pathway. The modules are interconnected in a sequence so that they flash on and off in a pattern that leads the driver or observer along a path with less confusion than with randomly flashing or steady lights or reflectors. The modules are self-powered and can be arrayed first and programmed following deployment. The programming can be done with “mesh” technology, an external controller, or by dialing a specific number in each of a plurality of distributed controllers. The modules can improve highway safety by reducing driver confusion. The modules are arrayed to prevent a driver from seeing them from an oncoming direction. The driver coming from the opposite direction will have his or her own guiding system.

Abstract: Disclosed are a metal fm pipe foundation apparatus and method for airport approach lighting and method of making, using, and installing a metal fin pipe foundation for airport approach lighting. The metal fin pipe foundation (MFPF) of the present invention requires a small 16 inch diameter hole to be drilled approximately 8 feet deep. The MFPF, in one aspect, consists of 16 inch diameter schedule 30 pipe 6 feet long with two (2) ? inch thick flat plate fins which are 6 feet in length, and which are welded to the 16 inch schedule 30 pipe. A top plate 5 feet in length, 1 foot 6 inches in width, and ¾ inch thick is attached by welding the top plate to the top of the 16 inch pipe and the top of the ? inch fins After the MFPF of the present invention is completely fabricated, it is dipped in hot galvanizing to protect the raw steel. This coating of galvanizing protects the MFPF for 75 years. The MFPF of the present invention can be fabricated off site and shipped to the airport ready for installation.

Abstract: A display system for an aircraft includes a processing unit configured to determine a touchdown point for the aircraft and to supply display commands associated with the touchdown point; and a display device coupled the processing unit and configured to receive the display commands and operable to render symbology representing the touchdown point.

Abstract: Precision approach path indicator systems (PAPIs) effective in providing approach slope guidance for aircraft approaching an airport runway are provided. Such PAPIs include a plurality of light assemblies positioned on or in proximity to an airport runway and structured or configured to be effective in providing approach slope guidance light signals to a pilot of an aircraft approaching a runway. Each light assembly includes a light source comprising light emitting diodes (LEDs), preferably a first array of LEDs and a second array of LEDs.

Abstract: A visual navigational aid for guiding the approach path of incoming aircrafts, ships or other vehicles. The visual navigational aid comprises high intensity light emitting diodes (LEDs) or LED arrays and optical beam shaping apparatus that produce multiple light beams with different colors or flash patterns to guide the incoming aircrafts, ships or other vehicles to a pre-determined approach path.

Abstract: A method and a device are described for acquiring driving data of a vehicle. Moreover, a computer program and a computer program product are put forward for carrying out the method. In the method described, a three-dimensional, kinematic vehicle model is calculated, including linear-motion-dynamics signals and lateral-motion-dynamics signals. This model can be utilized for reconstructing the vehicle movement.

Abstract: System for displaying on a first moving object a position indication dependent on a position of a second moving object. The system (1) comprises measurement means (2) for carrying out position measurements relating to at least one position dependent on the second moving object, processing means (3) mounted on the first moving object, and connected to the measurement means (2), and intended for the processing of said position measurements so as to produce a characteristic position, a display device (4) mounted on the first moving object, connected to the processing means (3), and presenting on a viewing screen (6), on a display illustrating at least partially the environment of the first moving object, a position indication which is situated at said characteristic position, and triggering means (7) for triggering the implementation of measurements by said measurement means (2).

Abstract: A beacon system includes emitter devices, driver circuitry configured for controlling the emitter devices, and at least one processor programmed to receive and process one or more inputs and control the driver circuitry to actuate the emitter devices. In an example embodiment, the emitter devices include visible light sources that are oriented to provide omni-directional visibility for the beacon system. In an example embodiment, components of the beacon system including the emitter devices, driver circuitry and at least one processor are configured such that in a space environment heat generated by the beacon system is dissipated sufficiently well to prevent the beacon system from overheating.

Abstract: The invention relates to a method for assisting the piloting of an aircraft in the vicinity of a landing or takeoff point, by: determining the locus of entry and/or exit points for a given approach and/or departure altitude that are not safe for reaching the landing and/or takeoff point; and presenting a diagram including said locus on a display device.

Abstract: A system for detection of foreign objects on airport travel surfaces including a plurality of foreign object detector modules mounted on a corresponding plurality of existing aircraft travel surface lighting supports, the plurality of foreign object detector modules providing a corresponding plurality of detection outputs and a high speed detection output analyzer operative to receive at least one of the plurality of detection outputs and to provide a high speed output indication of foreign object presence.

Abstract: Method and apparatus for providing visible indication of elevated airport light color during a non-operation condition. A set of light emitting diodes (LEDs) can be assembled to a housing of an elevated airport light. The housing and the set of LEDs can be covered by a clear glass, wherein the clear glass can be designed to cover some or an entire external region of the housing. Multiple colored tapes can be applied to a vertical portion of the housing such that, for example, a minimum of two-and-half square inches of the tape is visible from different angles. Therefore, the colored tapes can provide a clear visible indication of the elevated airport light color during a non-operation condition without the need for expensive colored glass and/or lens.

Abstract: A system and method for producing a flash of a desired intensity and duration utilizing devices of a lower intensity, such as light emitting diodes (LED's). The on period of the LED is lengthened so that the product of the LED's intensity and the on period is approximately equal to the product of the desired intensity and duration of the flash. A parameter for determining intensity, such as operating current or voltage, can be measured and the on period can be adjusted accordingly. The device can be turned on responsive to an external trigger signal, and a timer can be utilized to turn the device on if the external trigger signal is not received within a predetermined time.

Abstract: The invention relates to a method to help a person responsible for a vehicle on an airport to follow running procedures in the airport, the vehicle including a device for using the method, including: a database including: data modelling all or some of an airport environment; one or several acquisition devices for acquiring procedures applicable to the running operation on the airport; one or several devices configured to acquire and determine vehicle status information; calculation means using the database; graphic transcription means and warning means; means of generating sound and visual alarms; wherein the assistance method includes at least the following steps: determine applicable procedures; continuously calculate deviations between the behaviour of the vehicle and applicable procedures; graphic transcription of progress of the vehicle while running and deviations from applicable procedures; trigger visual and/or sound alerts when a predetermined deviation threshold is crossed.

Abstract: An apparatus for aligning an aircraft with an area on the ground is provided. The apparatus includes an aircraft having an on-board landing system, the on-board landing system configured to record an image of an area on the ground. The apparatus also includes a location marker on the area of the ground, and a stored image showing at least a portion of the area of the recorded image. The on-board landing system is configured to obtain information from the location marker and use the information to align the recorded image with the stored image.

Abstract: The invention is directed to a method for determining an optimal runway lighting intensity based on the determination of an optimal lighting intensity for a configurable target value of the runway visual range taking into account the runway-specific parameters of the lighting system, the meteorological optical range, and the background brightness. It is the object of the invention to provide a method by which it is possible to significantly reduce the energy consumption of a runway lighting system by specific control of the energy supply from economic and ecological view points and by fully taking into account all safety-related aspects.

Abstract: A system to identify junctions of restricted areas to approaching vehicles, including at least one warning signal generator, at least one antenna coupled to the generator transmitting the warning signal into areas traversed by the vehicles approaching the restricted areas, a receiver in each of the vehicles receiving the transmitted warning signals when the vehicle approaches one of the restricted areas, and an alarm responsive to the warning signal, which produces an alarm signal detectable by a vehicle operator.

Abstract: Precision approach path indicator systems (PAPIs) effective in providing approach slope guidance for aircraft approaching an airport runway are provided. Such PAPIs include a plurality of light assemblies positioned on or in proximity to an airport runway and structured or configured to be effective in providing approach slope guidance light signals to a pilot of an aircraft approaching a runway. Each light assembly includes a light source comprising light emitting diodes (LEDs), preferably a first array of LEDs and a second array of LEDs.

Abstract: A navigation apparatus with image recognition, includes: an imaging section for obtaining a stereo image of a target spot; an inertial information detecting section for measuring an attitude angle of a body and an acceleration of the body; an image process calculating section for calculating a relative position of the body with respect to the target spot based on the stereo image and the attitude angle; and a navigation calculating section for calculating navigation information based on the attitude angle, the acceleration and the relative position.

Abstract: An aircraft emergency lighting system includes a plurality of light units arranged to guide passengers to and to identify exits in an emergency. The light units communicate wirelessly with a remote master control unit operable from the cockpit using a low power spread spectrum signal centered on a single frequency to avoid interference with onboard aircraft control and communication systems. The light units are arranged to receive and transmit any signal to and from the master controller whereby only some of the light units need be within range of the master controller. The light units include battery operated LEDs and cycle between an inoperable (sleep) condition and an operable (awake) condition to conserve power consumption and extend battery life.

Abstract: An aircraft flight control display for orientation of the pilot during an approach of the aircraft toward a destination has a center of the display as its fixed point. An aircraft symbol with a center depicts the longitudinal axis as well as a lateral line to depict the current attitude of the aircraft. A destination position symbol has a reference line and a position symbol, with a skyline having a center. The destination position symbol is located at a distance from the center and its reference line points to the center as the reference point. The destination position symbol is rotated around the reference point dependent on the relative position of the aircraft's direction or the flight direction to the desired destination direction.

Abstract: A warning system for a wind power installation of a wind farm. In one embodiment, the warning system comprises a visibility measuring device. In one embodiment, the warning system comprises a controller configured to synchronize flashing lights on the wind power installation with flashing lights on another wind power installation of the wind farm.

Abstract: A vision system and method for use on a refueling tanker to assist a boom operator in performing an airborne refueling operation on a receiver aircraft. The system includes a digital camera system, a sensor subsystem and a processing system that receives information from the sensor system and the camera system. The processing system includes video processing capability and a graphics generator that generates a two dimensional graphics symbology set that is displayed on a display terminal along with a real time image of the boom and the receiver aircraft. The graphics symbology set includes a plurality of graphic symbols that indicate the position of the refueling boom and the position of the receiver aircraft relative to a desired contact zone within which physical contact between the boom tip and a refueling receptacle on the receiver aircraft can be made. The graphics symbology set also makes use of various colors to indicate warning conditions to the boom operator.

Abstract: A vision system and method for use on a refueling tanker to assist a boom operator in performing an airborne refueling operation on a receiver aircraft. The system includes a digital camera system, a sensor subsystem and a processing system that receives information from the sensor system and the camera system. The processing system includes video processing capability and a graphics generator that generates a two dimensional graphics symbology set that is displayed on a display terminal along with a real time image of the boom and the receiver aircraft. The graphics symbology set includes a plurality of graphic symbols that indicate the position of the refueling boom and the position of the receiver aircraft relative to a desired contact zone within which physical contact between the boom tip and a refueling receptacle on the receiver aircraft can be made. The graphics symbology set also makes use of various colors to indicate warning conditions to the boom operator.

Abstract: A system for detection of foreign objects on airport travel surfaces including a plurality of foreign object detector modules mounted on a corresponding plurality of existing aircraft travel surface lighting supports, the plurality of foreign object detector modules providing a corresponding plurality of detection outputs and a high speed detection output analyzer operative to receive at least one of the plurality of detection outputs and to provide a high speed output indication of foreign object presence.

Abstract: An improved system and method are disclosed for indicating the validity of airport runway visual approach slope indicators on an aircraft display. An aircraft display system is provided, which includes a database for storing data about the specific visual approach slope lighting indicator system being used by each airport of a plurality of airports and any special distance and/or usage limitations associated with each such visual approach slope indicator system, a processing unit, a position determination unit, and a visual display. As an aircraft approaches an airport, the processing unit receives the aircraft's current position from the position determination unit, and compares the aircraft's current position data with the distance and/or usage limitation data stored in the database for the approach slope indicator system being used by that airport.

Abstract: Remote monitor and control of an airfield lighting system. A processing system local to the airport is provided in communication with the airfield lighting system for monitor and control thereof, the airfield lighting system producing airfield information for processing by the local processing system. The local processing system connects to a global communication network such that the airfield information is accessed from a remote location disposed on the global communication network.

Abstract: A method and system for visually guiding an aircraft in its landing approach to a runway having an approach area equipped with approach lights operable in off, low, medium, and high intensity states. The lights are communicated with a secondary side of a transformer, which has a primary side with low, medium, and high taps that correspond to the light states. Off, low, medium, and high lighting intensity requests correspond to the low, medium, and high states of the plurality of lights. AC power is switched between the transformer taps in response to a request for an increase in lighting intensity. Power is sequentially applied to the taps by supplying the power to the low tap for a first predetermined time interval before supplying the power to the medium tap.

Abstract: A method and system for visually guiding an aircraft in its landing approach to a runway having an approach area equipped with approach lights operable in off, low, medium, and high intensity states. The lights are communicated with a secondary side of a transformer, which has a primary side with low, medium, and high taps that correspond to the light states. Off, low, medium, and high lighting intensity requests correspond to the low, medium, and high states of the plurality of lights. AC power is switched between the transformer taps in response to a request for an increase in lighting intensity. Power is sequentially applied to the taps by supplying the power to the low tap for a first predetermined time interval before supplying the power to the medium tap.

Abstract: A runway lighting fixture of the type normally permanently installed at an aircraft installation such as an airport to provide visible light signals to an aircraft, the fixture having an internal, non-visible light source such as an infrared lamp capable of being activated to provide a non-visible light signal to an aircraft specially equipped to see such non-visible signals. An airport normally having arrays of permanent visibly-lighted fixtures can be equipped for long-term or permanent covert operations capability by installing covert, non-visibly-lighted fixtures in place of visibly-lighted fixtures. In a preferred form the covert fixtures are capable of being both visibly and non-visibly lighted to allow normal appearing non-covert operations at the airport, and unobtrusive covert operations whenever needed.

Abstract: A flat panel display system for an aircraft display includes a graphics rendering computer for rendering of anti-aliased graphical imaging data derived from aircraft sensors for full-field imaging on a cockpit display screen. A comparator processor independently generates, from the same sensor data, a selected subset or “points of light” of the display screen image and compares the points of light data to the data generated by the rendering computer for the same display screen pixel locations. The minimized processing requirements and simplified design of the comparator processor enable ready FAA certification of the comparator processor, whereas the extreme complexity and processing operations required of the rendering computer make FAA certification thereof unusually time consuming and expensive.

Abstract: An illumination system has a mounting plate, a plurality of thermally conductive circuit boards in thermal contact with the mounting plate, a plurality of light emitting diodes electrically and thermally communicating with the circuit board strips, an optical lens formed as a translucent dome covering the circuit boards and light emitting diodes, and a lamp base operatively coupled to the mounting plate and circuit boards. The light emitting diodes receive power from an external electrical source entering the system through the base and the circuit boards.

Abstract: An airfield guidance sign. The sign 100 (of FIG. 1a) includes a case (102), a multi-element light source (114) attached to the case (102) for providing light interior to the case (102), a light dispersion subsystem of the case for dispersing the light from the light source (114) substantially uniformly throughout the interior of the case (102); and a side panel (126) forming a side of the case (102) for displaying information.

Abstract: A system for detection of foreign objects on airport travel surfaces including a plurality of foreign object detector modules mounted on a corresponding plurality of existing aircraft travel surface lighting supports, the plurality of foreign object detector modules providing a corresponding plurality of detection outputs and a high speed detection output analyzer operative to receive at least one of the plurality of detection outputs and to provide a high speed output indication of foreign object presence.

Abstract: The invention is a method for displaying otherwise unseen atmospheric phenomenon using augmented reality (the mixing of real media with computer generated media). The method uses computer generated images to represent existing weather conditions and presents this data to the user by combining the computer generated images with the user's real environment. Computer generated images are used to represent such weather phenomenon as wake vortices, wind shear, and microbursts. These images are represented in such a way as to intuitively display relevant properties of the phenomenon to the system user, which increases the user's situational awareness and safety. The primary intended applications are for air traffic controllers and pilots to view these disturbances.

Abstract: The object of the invention is to improve a flight warning light arrangement of wind power installations and in particular to make the operation thereof as effect as possible. Disclosed is a flight warning light arrangement for a wind power installation, comprising at least one light means which is mounted on the wind power installation, wherein there is provided a device for detecting the brightness value, for example a twilight switch which detects the level of daytime brightness in the area around the wind power installation, and the device for detecting the brightness value is connected to a switching device which evaluates the measured data and switches on the flight warning light arrangement when the brightness value falls below a given value.

Abstract: A radio tower light system utilizes a ground-level semiconductor optical light source and includes fiber optic cabling that is strung along the tower to the various desired locations for the beacon light. A lens system, at each beacon site, is coupled to the termination of a fiber optic cable and used to magnify and radiate the optical signal in the desired direction. The use of a ground-based light source eliminates the need for a technician to climb the tower (or lower the beacon) upon failure of the light source.

Abstract: An airfield guidance sign. The sign 100 (of FIG. 1a) includes a case (102), a multi-element light source (114) attached to the case (102) for providing light interior to the case (102), a light dispersion subsystem of the case for dispersing the light from the light source (114) substantially uniformly throughout the interior of the case (102); and a side panel (126) forming a side of the case (102) for displaying information.

Abstract: A monitoring and control system controls multiple lights and monitors their operation through two-way communication over power lines. An interface is connected to receive control signals for at least one of the lights from the central computer and to transmit monitoring data concerning the lights to the central computer. The interface communicates over the power lines with light controlling and monitoring devices in the field to transmit the control signals over the power lines to the light controlling and monitoring devices and to receive the monitoring data over the power lines from the light controlling and monitoring devices.

Abstract: In an arrangement for supervising and controlling field light units (20) at an airport, a regulator provided with a monitoring unit for power supply and for monitoring the light units is arranged individually for each light unit (18,20) to regulate the light intensity of the light units and to receive information as to their operational status. In a preferred embodiment, each light unit comprises two separate light sources that can be alternately and separately connected into circuit in case of failure to either of the light sources. Each light unit is provided with an electronic unit including a regulator, monitoring unit, and modem for power supply to the light unit and for monitoring the operation of the light unit. Each light unit is individually addressable from a control central for the airport. A ground traffic control system can be integrated into the field lighting system by connecting suitable presence detectors to the system.

Abstract: An LED array warning light system comprises a plurality of struts in a generally conical configuration. Each strut has an upper and lower edge and an inner and an outer edge. A plurality of light emitting diodes are affixed one above the other to an edge of each strut. A top disk with radial slots receives and is affixed to an upper edge of an associated strut. A bottom disk has radial slots which receive and are affixed to a lower edge of an associated strut. The disks are sized whereby the LED's are at an angle of between 3 and 25 from the axis.

Abstract: A portable landing aid apparatus is disclosed along with a method for operation in aiding a pilot of a helicopter to land the helicopter in adverse conditions, such as at night or in inclement weather, at a non-traditional landing site. The landing aid apparatus comprises a plurality of light units that are powered by a portable power supply, such as a battery or an emergency vehicle at the site. Each light unit further includes a white strobe light, a steady burn amber lamp, and a green strobe light. The white strobe light is utilized as a day locator, while the green strobe light is utilized as a night locator. The steady burn amber light is used as a landing locator. The white strobe light is utilized during the day as it is highly visible from long distances and does not interfere with the pilot's vision. The green strobe light is used at night as it is highly visible at night and does not interfere with the pilot's night vision.

Abstract: A light weight, self-contained, portable, intrinsically-safe warning device for providing warning to personnel of an unsafe condition is provided. This warning device is especially adapted for attachment to the roof of a mine to indicate unsupported roof conditions or other unsafe conditions.

Abstract: FAA regulations mandate that a pilot must have sufficient visibility to see the airport, and then the runway before landing; and sufficient visibility to see a substantial portion of the runway before taking off. In adverse weather conditions when visibility is reduced flights are cancelled, delayed, and rerouted to land where visibility is adequate. Poor visibility is one of the major causes of air traffic fatalities. One aspect of this invention discloses a method of illuminating an aircraft landing location to facilitate identification and aircraft guidance thereto comprising the following steps: projecting a laser beam upwardly from the location so that an aircraft may be better able to target the landing location particularly in conditions of poor visibility.

Abstract: A power-line carrier airport facilities monitor system, comprising a host station and respective terminal for monitoring individually the object facilities via a rubber transformer are connected in series to a power line derived from a fixed current generator, wherein the host station and respective terminal create a control command for respective terminal/monitoring signal of the object facilities as text data and, on the other hand, injections said text data to the power line by FSK modulation based on the zero cross detection of the power line power source waveform.

Abstract: The present invention relates primarily to an aircraft approach and landing system using passive retroreflective panels strategically placed along both sides of a landing strip or runway. The retroreflective panels comprise pairs of color-coded orange panel markers indicating the touchdown zone and singly, the remainder of the landing strip. The array of reflective elements are placed adjacent to the runway path so that the array produces a left/right reflected beam envelope within which an aircraft may be centered in order to maintain a desired landing vector. Upon installation of the reflector panel elements, each panel can be tilted with respect to the runway surface at an angle corresponding to the glide slope to produce a visual reflective beam aligned to the desired glide slope angle.

Abstract: A laser lighting system of beam shaping, delivery, and the retroreflection of laser light on specially designed markers to reduce the problems associated with the illumination of markings, signage, and reflectors installed in northern climates. The laser lighting system employs employ visible and reflective laser beam lighting sources to provide illumination of airport runways and taxiways, preferred approach and departure routes, seaplane base landing areas, marine waterways, as well as to assist in search and rescue operations. The laser lighting system may be a laser lighting post or a laser lighting unit for providing radiation along a surface that includes at least one laser for producing a beam of coherent visible or reflective radiation, and a glass plano-convex cylindrical lens which has an aspherical convex cylindrical surface for generating a laser line which is uniformally illuminated from end to end.