Abstract: An active noise control system for aircraft includes a headset for use by a pilot of the aircraft. A plurality of sensors are mounted on the aircraft at predetermined locations to sense aircraft noise. The aircraft noise at each of the sensors has a first sound waveform in a first phase. A plurality of actuators are operatively connected to respective sensors and communicate with the headset. Each actuator generates a second sound waveform in a second phase. A controller commands each of the plurality of actuators, and dictates the second phase of the second sound waveform, such that the first and second sound waveforms interact out of phase in a manner sufficient to control the aircraft noise. The controlled aircraft noise enables auditory detection of remote environmental disturbances outside of the aircraft thereby enhancing pilot sensory awareness.

Abstract: The invention concerns a method and a system for calculating a flight route between a first position and a second position. According to the method, the first position is chosen as the current position, and the following steps are then repeated until the second position is reached: a loss function is determined corresponding to each flight path in a set of flight paths that are predefined in relation to the current direction of flight; a flight path that yields the most advantageous value for the loss function is selected; a subsection from the current position and a predetermined number of positions forward are registered for the selected flight path, and the position at the end of the subsection is chosen as the new current position.

Abstract: A safe interactive navigation apparatus and method allows the crew of an aircraft to prepare and follow a safe flight plan without relying on instrument flying infrastructure. An aircraft navigation assistance method calculates a continuous, three-dimensional projected path on board the aircraft as a function of data related to the route and characteristics of the aircraft.

Abstract: A method and apparatus for controlling a plurality of solar panels of a spacecraft is described. The method comprises the steps of providing a first step command to a first solar panel, and providing a second step command to a second solar panel at a time of a transient zero-crossing of a dynamic response of the spacecraft body to the first step command, wherein the second solar panel is disposed on an opposite side of the spacecraft from the first solar panel. The apparatus comprises a processor; a first solar panel driver, communicatively coupled to the processor, for providing a first step command to a first solar panel, and a second solar panel driver, communicatively coupled to the processor, for providing a second step command to a second solar panel at a time of a transient zero-crossing of a dynamic response of the spacecraft body to the first step command.

Abstract: The invention relates to methods and devices for aircraft's safe operation and is embodied in the form of a method and system for informing a user, for example an aircraft crew and/or a flight controller, on the probable penetration of the aircraft into dangerous areas of the vortex shedding of vortex generators which are located near the aircraft at a forecast time when the aircraft passes through a simulated control plane situated at a preventive distance in the direction of motion of the aircraft, said distance being calculated on a basis of a sufficient forecast period so that the aircraft carries out a flight evasive manoeuvre.

Abstract: Conventional terrain anticollision equipment formulates, around the short term forecast trajectory of the aircraft which is equipped therewith, virtual volumes of protection of maneuver charted by feelers and signals a risk of terrain collision as soon as it detects an intrusion of the terrain into these virtual volumes of protection of maneuver.

Abstract: A system and method of automatically advising an individual, in real-time, of all available facts related to a current situation. The method is facilitated by a system, which automatically retrieves data related to a situation from a plurality of aviation enterprise systems, processes the data retrieved in real time and generates a situational awareness data that is presented in an optimal format to a user on an interface device. Processing of the data retrieved from the plurality of aviation enterprise systems comprises correlating the data in accordance with business rules and interpreting the data in view of previously stored historical information that relates to the situation. The situational awareness data generated is further processed in view of a user profile in order to create a viewable situational awareness data that has been optimized for presentation to an identified user of the system in accordance with the user profile.

Abstract: A method and system for determining a location of a vehicle, the method comprises determining reception location data within a first cell of a work area for a vehicle. A reception quality estimator estimates reception quality data for the corresponding reception location data for the first cell. Optical location data is determined within a first cell of a work area for a vehicle. An optical quality estimator estimates optical quality data for the corresponding optical location data for the first cell. A data processor selects at least one of the reception location data and the optical location data as refined location data associated with the first cell based on the estimated reception quality data and estimated optical quality data.

Abstract: An E-field sensing system is provided to detect the presence of obstacles, including wires, power lines or trip wires, as well as towers, guy wires, buildings and elevated terrain, in which a variation or tilt of the iso-potential electrostatic field adjacent the obstacle is detected. In one embodiment the bearing to the obstacle is ascertained. The result is the detection of power lines from as far away as at least 1,000 feet and unpowered wires from as far away as at least 100 feet, thus reducing pilot anxiety for low level missions as well as providing for wire strike avoidance.

Abstract: Method and device for determining the lateral path of a moving body, in particular of an aircraft. The device (1) comprises means (7) for determining, from a first lateral path and a lateral distance dependent on the external visibility, a second lateral path corresponding to the lateral path of the path, in particular a flight path, which is followed by the moving body.

Abstract: A helmet mounted tracking system for target designation includes an airplane azimuth sensor, a helmet mounted azimuth sensor, an airplane pitch sensor, a helmet mounted pitch sensor, and a processor. The airplane azimuth sensor determines an azimuth heading for an airplane. The helmet mounted azimuth sensor determines an azimuth heading for a helmet that is worn by a pilot. The airplane pitch sensor determines a pitch for the airplane. The helmet mounted pitch sensor determines a pitch for the helmet that is worn by the pilot. The processor is in operative communication with the airplane azimuth sensor, the helmet mounted azimuth sensor, the airplane pitch sensor, and the helmet mounted pitch sensor and the processor is processes instructions from each of the sensors to determine a target pitch and a target azimuth.

Abstract: A testing apparatus for determining the enhanced vision capabilities of a system that is designed to assist a pilot in detecting lights and ground features in night and low visibility conditions. One embodiment of the apparatus is suitable for laboratory or production facilities, the other embodiment is used for the flight line by installing it in the aircraft. A simulated pattern is presented by the apparatus wherein the enhanced vision system (EVS) can be calibrated. Further, fog can also be simulated over the spectral band of the EVS. Runway landing lights are also able to be simulated using a readily available light source.

Abstract: An airplane system on an airplane is for use in a turbulence analysis system. The airplane system comprises a communication interface, a processing system, and a user interface. The communication interface receives satellite signals from a plurality of satellites. The processing system processes the satellite signals to determine time variance metrics that correspond to variances in signal transfer times for individual satellite signals. The communication interface transfers the time variance metrics for the satellite signals. The time variance metrics are received by the turbulence analysis system. The communication interface receives at least a portion of a turbulence map into the airplane system. The turbulence map is generated by the turbulence analysis system based on the time variance metrics and indicates atmospheric turbulence in a three-dimensional area. The user interface displays the portion of the turbulence map.

Abstract: A method for balancing vibrations in a rotating machine is provided. The rotating machine has a first and a second plane of imbalance. The method includes determining a first set of solution mass vectors that includes a first solution mass vector for the first plane and a first solution mass vector for the second plane. Each first solution mass vector includes a mass and a phase angle. A first phase difference between a phase angle of the first solution mass vector for the first plane and a phase angle for the first solution mass vector for the second plane is calculated. The first phase difference is compared to a pre-selected value. If the first phase difference is less than the pre-selected value, the first set of solution mass vectors is retained. The first set of solution mass vectors is then incremented to create a second set of solution mass vectors that includes a second solution mass vector for the first plane and a second solution mass vector for the second plane.

Abstract: A system and method are provided for the efficient entry and display of ground taxi routes on an electronic airport map display. The system may include a touchscreen entry device, a display device, a computer, a map database, a vehicle position sensor and a transmitter/receiver. The system may be configured to check the ground taxi entries to ensure that each successive segment is contiguous with the last or next segment, and any gaps or discontinuities in the displayed taxi instructions may be annunciated. An intelligent display of next possible segments may be incorporated into the system.

Abstract: A system for supervising the speed of at least one engine of an aircraft includes three independent information sources determining first, second and third values for an aerodynamic parameter of the aircraft and precision information indicating the precision of these values. A control unit acts on the operation of the engine, and a sensor measures a fourth value for the parameter. An arithmetic unit selects a control value by using the first, second, third and fourth values of the aerodynamic parameter and the precision information and uses the control value to determine a control sequence for the control unit. An information transmission network, to which the three independent information sources and the arithmetic unit are connected, permits a transmission of information between the sources of information and the arithmetic unit.

Abstract: Systems and methods are disclosed that include a user interface that enables a user to request a pre-defined report. The user may specify either or both of an electronic mail delivery address for the report and an interval at which the report is to be updated. Such systems and methods enable a particular report to be produced and formatted only once, and then provided to multiple users, thereby eliminating the production and formatting of redundant reports.

Abstract: A method and system which allow a user to define and edit workflow applications for a mobile device, screens associated with the applications, and workflow process is described. The states or schemas for these applications may be stored as records in databases.

Abstract: A portable, handheld electronic navigation device includes an altimeter and a GPS unit. An internal memory stores cartographic data, for displaying the cartographic data on a display of the navigation device. Accordingly, the device is capable of displaying cartographic data surrounding a location of the unit as determined by GPS and altitude information as determined by the barometric altimeter and GPS. The device provides an enhancement of the calibration and hence the accuracy of barometric altimeter measurements with the aid of derived altitudes from a GPS. The device is able to determine the need for calibration and perform the subsequent computations necessary to facilitate the calibration. Furthermore, the device is able to determine a correction quantity that should be applied to barometric altitude readings, thereby allowing the device to be calibrated while in motion. Both of these features ultimately result in a more accurate determination of altitude.

Abstract: A system and process for countering the vibrations induced in an aircraft by the windmilling of an engine fan may produce a first electric flight control command for a servocontrol to use in actuating a control surface of the aircraft. The servocontrol is slaved to the first electric flight control command, and the servocontrol's operation is limited to a reduced frequency band. Vibrations induced by the windmilling of the engine fan are monitored, and, when the monitored vibrations exceed a threshold, a second electric flight control command for application to the servocontrol is computed to oppose the induced vibrations. Also, the first and second electric flight control commands are summed to produce an overall control command for the control surface, and the servocontrol is temporarily slaved to the overall control command for operation in a widened frequency band.

Abstract: In the case where variations in ground objects in one and the same area are detected between a line drawing map describing profile lines of the ground objects or a reference line drawing/image obtained by picking up the ground objects from above, and a target image obtained by picking up the ground objects in the same area from above later on, a variation detecting apparatus collates the reference line drawing/image with the target image so as to obtain variation indexes indicating whether there are variations or not in the ground objects respectively, and displays ground objects which can be judged to have variations or ground objects which cannot be judged as to whether there are variations or not on the basis of the variation indexes, in a display mode in which an area of the reference line drawing/image including the ground objects and an area of the target image including the ground objects can be compared with each other.

Abstract: An apparatus for measuring and fixing the three-dimensional location of medical instrument that can be easily placed at a desired location by a user. In addition, a medical apparatus for measuring the three-dimensional locations of an apparatus fixed at an end portion of a cancer and an external apparatus and fixing the apparatus at an end portion of the cancer, which can be easily placed at a desired location by a user and carries out the location-fixing and measuring at the same time. The apparatus is applicable for various medical fields such as the measurement of the location and orientation of an external apparatus, the measurement of relative locations of a medical instrument contacted to an end-portion of a cancer and the object body, and the fixation of the instrument at a desired location.

Abstract: Apparatus for controlling the power output efficiency of a power generation system based on an operator input. A processor is coupled to the input means and (i) receives the generated operator command, (ii) receives a plurality of detected ambient air conditions, (iii) receives a plurality of detected engine performance parameters, (iv) determines first and second engine control commands based on the received pilot thrust command, the detected ambient environmental conditions, and the engine performance parameters, and (v) outputs control commands to optimize the efficiency of the power generation system.

Abstract: A flight guidance system providing perspective flight guidance symbology using positioning and terrain information provides increased pilot situational awareness of the pilot's aircraft. The guidance system uses a positioning system and a detailed mapping system to provide a perspective display for use in an aircraft. A precision pathway flight guidance (PFG) symbology set is thereby displayed on a pilot display. The PFG symbology set includes broken line symbols representing an open tunnel and providing flow field data, a half-bracket symbol to indicate that the aircraft is no longer in the open tunnel represented by the broken line symbols and a quickened flight path vector (QFPV) symbol to provide the pilot with predictive flight path information. A flight director system and tunnel generator component provide for updating the displayed PDFG symbology set based upon current aircraft conditions (e.g., aircraft position) and stored flight path information.

Abstract: The present invention relates to a system and to an arrangement for evaluating in a defined space or area a delimited area (7) in which there is a degree of urgency greater than the degree of urgency in respect of the remainder of said space (1), wherein there is disposed within said space or area (1) a plurality of sensors which can evaluate the current or ongoing degree of urgency on the basis of one or more criteria. Selected sensors (2, 3, 4) shall be connected to computer equipment (50) which includes storage elements (52, 53, 54) adapted for storing current criteria-related values in a chosen time order, and wherein a calculating circuit (51) included in or connected to said computer equipment (50) is adapted for evaluation of a calculated degree of urgency on the basis of time-dependent changes in the evaluated current values, and determining and establishing the local orientation or geographic location of the delimited area through the medium of the calculating circuit.

Abstract: This invention control system having: means (12) for detecting an irregularity in aircraft handling during flight; means (18) for causing temporarily a rigid body excitation in at least a portion of the aircraft; means (20) for monitoring an actual response to the excitation; means (22) for comparing the actual response and a target response to the rigid body excitation; and means (14) responsive to an output from the comparison means for determining the need for a modification of the current flight plan and for generating a corresponding control output. The invention also provides a corresponding method for controlling an aircraft.

Abstract: An apparatus and network, each including at least one expansion module, and an associated method are provided. The expansion module can be disposed between an aircraft connector and an avionic device connector to provide an electrical circuit for transmissions therebetween. The expansion module generates a signal representative of the transmissions, and the signal can be communicated, for example, via an Ethernet network to a controller, data storage device, or other devices. Further, the expansion module can be received by a tray that is also configured to receive the avionic device, so that the tray secures the avionic device to the aircraft, and the expansion module connects the avionic device and the aircraft when the avionic device is received by the tray. The expansion module can be disposed between corresponding aircraft connectors and avionic device connectors, such that the present invention can be used to retrofit existing aircraft.

Abstract: The present invention provides an aircraft navigational system including a graphical user interface that is capable of displaying navigational information in a split-screen format. The split-screen format includes displaying multiple graphical user panels, each depicting different traffic information. For example, one of the panels displays a plurality of air traffic symbols corresponding to airborne obstacles and another of the panels simultaneously displays ground traffic symbols representing ground obstacles. The obstacles can include other aircraft in the air and on runways as the pilot's aircraft approaches for a landing. The navigational system also is capable of switching between a single graphical user panel and multiple panels in response to a triggering event, such as a change in the course of the aircraft.

Abstract: A mandatory access control system and method that employs a policy manager subsystem with virtual data labeling (VDL) on the communications channel to allow aspects about the data to determine by whom and where such data can be accessed. When combined with a secure network system, the VDL system is able to base delivery decisions not only on destination address but also on the type of data that is to be delivered.

Abstract: A terrain clearance measuring radio wave being emitted from an airplane is received, and changes in electric field intensity of the radio wave is input and recorded to a computer, whereby the time of occurrence of a sharply appearing peak value of the changes permits accurate measurement of the point-blank passing time, independent of flight frequency.

Abstract: A system allowing for an integrated flight loads balancing process at one or more time instances of a flight maneuver of an aircraft includes a processor and a plurality of resources. Additionally, the system includes a resource integration program that is executable by the processor. Upon execution by the processor, the resource integration program operates to integrate the plurality of resources so that the integrated resources are accessible to the system while balancing the flight loads at the one or more time instances.

Abstract: An airborne computer is linked to a ground-based or satellite-based supplier of weather data that is geographically referenced. The computer retrieves the weather data on a regular cycle but does not display the data. The computer also has access to the aircraft's state, i.e., position, altitude, speed, and intended route. Algorithms within the computer combine the present and estimated future positions of the aircraft with the weather data, and create an alert to the crew if a threat is detected. When a threat is detected, the weather display is activated to draw the attention of the crew to the threat.

Abstract: The invention concerns a method for preventing airplanes from impermissibly approaching defendable ground objects, with the momentary flight position being recorded in a satellite-based way and used for the purposes of manual and automatic flight corrections.

Abstract: Multiple data and images are multiplexed and sequenced in order to minimize the recording and monitoring hardware required to process the images, providing a detailed record of an event, greatly enhancing event reconstruction efforts. The multi-media safety and surveillance system for aircraft incorporates a plurality of strategically spaced sensors including video imaging generators for monitoring critical components and critical areas of both the interior and the exterior of the aircraft. The captured data and images are recorded and may be transmitted to ground control stations for real time or near real time surveillance. The system includes a plurality of strategically located video image sensors such as, by way of example, analog and/or digital video cameras, a video data recorder (VDR) and a pilot display module (MCDU or MIDU). All data is in recorded in an IP format. The IP encoder may be an integral component of the VDR, or the data may be transmitted in an IP format from the data generator device.

Abstract: A method of generating a synthetic pressure altitude is disclosed. The method includes providing a static air temperature to a data processing device. The method also includes providing a wind velocity, a ground velocity, and a geometric altitude to the data processing device. Further, the method includes performing a numerical integration based on the static air temperature, the wind velocity, the ground velocity, and the geometric altitude. The wind velocity and the ground velocity are used to estimate pressure gradients not included in a static air column model.

Abstract: A lane recognition apparatus for recognizing lane markers on a road surface based on a pair of stereo images of a scene in front of an own vehicle obtained from a stereoscopic camera, includes a stereo image processing means for calculating distance information of an image based on the pair of the images, a lane detecting means for detecting a lane marker of a lane in the image based on brightness information of the image and distance information calculated by the stereo image processing means and a lane position recognition means for recognizing a position of the lane marker in real space based on a position of the lane marker detected by the lane detecting means and distance information calculated by the stereo image processing means.

Abstract: A noninvasive system for monitoring the oxygen saturation level of a person subjected to reduced atmospheric pressure for avoiding hypoxemia. The system monitors a person's oxygen saturation level, comparing the saturation level to a predetermined level. When the measured saturation level is less than the predetermined level, the person is then supplied with an oxygen mixture for increasing the subject's oxygen saturation level to a safe level. The person's exposed reduced atmospheric pressure is also compared with a predetermined range of pressure levels. If this predetermined range of pressure levels is exceeded or maintained for a predetermined time duration, the person is then supplied with an oxygen mixture. Additionally, a device is provided for performing oxygen flight planning calculations for estimating oxygen usage for a predetermined flight plan that is based on the above system.

Abstract: A noninvasive system for monitoring the oxygen saturation level of a person subjected to reduced atmospheric pressure for avoiding hypoxemia. The system monitors a person's oxygen saturation level, comparing the saturation level to a predetermined level. When the measured saturation level is less than the predetermined level, the person is then supplied with an oxygen mixture for increasing the subject's oxygen saturation level to a safe level. The person's exposed reduced atmospheric pressure is also compared with a predetermined range of pressure levels. If this predetermined range of pressure levels is exceeded or maintained for a predetermined time duration, the person is then supplied with an oxygen mixture. Additionally, a device is provided for performing oxygen flight planning calculations for estimating oxygen usage for a predetermined flight plan that is based on the above system.

Abstract: Method and device for reducing the vibratory motions of the fuselage of an aircraft. According to the invention, accelerometers (9, 10) are mounted on engines (M1, M4) of the aircraft (1) and, with the aid of the accelerometric measurements thus obtained and of the aeroelastic model of said aircraft, control commands (dZ, dY) to be applied to the ailerons (M1 to M4) so as to counteract the oscillations of said engines are determined.

Abstract: A grid terrain data collision detecting method for forward looking terrain avoidance comprising the following steps: the use of kinematics equation to analytically find out sampling points positions; processing the sampling points in sequence with time increments; and using function minimum value theory to detect collision with results obtained from the sampling point process step.

Abstract: Process and device for detecting the failure of a pressure sensor of an air data system of an aircraft.

Abstract: A spatial data search method, system and apparatus for identifying particular data of significance around a reference vector through the spatial data. The method involves determining a reference vector within a spatial region for which spatial data exists, loading a portion of the spatial data including the data around the reference vector into a memory buffer, and searching the spatial data in a prioritized order. The method, system and apparatus have particular utility in searching geographic data for a terrain awareness and warning system (“TAWS”) and display in an aircraft. Embodiments of the present invention provide advantages over existing sequential and radial search methods, significantly reducing the processing and calculations required and providing faster alerts to pilots.

Abstract: A method routes an entity (200) through a predetermined area for scanning the content of the predetermined area. The method comprises the steps of: partitioning the predetermined area into cells (100); determining a starting cell for the entity (200); initiating a scan of a number of the cells from the starting cell and determining the content of each of the number of cells; and determining a total cost for the entity (200) to travel to each of the scanned cells and to perform a scan from each of the scanned cells.

Abstract: A system for enhancing flight safety of a host aircraft receives an adjustment value from a portable memory device; determines a working value of a parameter in accordance with the adjustment value; and provides an advice for threat avoidance in accordance with the working value of the parameter, a terrain database, and an expected climb gradient capability of the host aircraft. The adjustment value may describe an adjustment to at least one of: an aircraft capability parameter, a flight crew capability parameter, a mission parameter, a threat detection technique parameter, a threat advice parameter, or a threat avoidance parameter. Threats include a risk of colliding with other aircraft, colliding with terrain, and encountering adverse weather conditions.

Abstract: In a multirobotic system comprised of automated mobile robotic vehicles (MRVs), a network of MRV drones provides sensor information to a lead MRV, which calculates the distance to objects in the environment. By using a method of optic flow to map coordinates in spatial positions, MRVs establish mission priorities and work as a group to accomplish a mission. Once the operational coordination is made for the group to organize its priorities and tasks, the enemy targets are struck in a sequence according to mission parameters.

Abstract: A system and method for detecting if a UAV is operating within its flight envelope. The invention includes defining the flight envelope of the UAV. The operating state of the UAV is identified from a present time to a future elapsed time. The invention determines if the UAV will be within its flight envelope at the end of the elapsed time in the future. It can then command the UAV to maintain operation within the flight envelope if the operating state determined is outside the flight envelope.

Abstract: Heterogeneous data at a plurality of remote nodes is accessed automatically in parallel at high speed from a user site using a simple script request containing a data source object name wherein the heterogeneous data is treated as a single data source object, the script further containing code representing a user-defined program to be executed on the data source object. The user-defined program may be represented by an embedded script, a user-defined script or an executable program designation. A user site agent breaks the user-generated script into new scripts appropriate for execution at the remote nodes. A messenger process transmits the new scripts to the appropriate remote nodes where respective agent processes respond to automatically access the appropriate data and to automatically execute the specified program. If the program is a user-defined script or executable, the respective agent processes access a metadata repository to obtain the specified program.

Abstract: A system, a method, and a computer program product for determining tactile cueing of a flight control input apparatus includes an interface for receiving observed parameters relating to the flight envelope of an aircraft. Upstream processing elements receive the observed states, convert dimensional aircraft state parameters into nondimensional aircraft state parameters, and provide the data to neural networks. The neural networks receive combinations of observed parameters and nondimensional aircraft state parameters and predict flight envelope limiting parameters. The neural networks are trained to predict the limiting parameters. A downstream processing element determines the most limiting flight envelope limiting parameter provided from the neural networks, therefore providing a tactile cueing position for a flight control input apparatus.

Abstract: A method and system for providing taxiway navigational information to a crewmember of an airplane taxiing at an airport. An airport taxiway navigation system (“ATNS”) that executes on an onboard computer system that displays a map of the taxiways of an airport, receives the name of each taxiway of the taxi route specified by the taxi clearance, and highlights the taxiways on a displayed map to provide a visual indication of the cleared taxi route for the crewmembers.

Abstract: A method routes an entity (200) through a predetermined area for scanning the content of the predetermined area. The method comprises the steps of: partitioning the predetermined area into cells (100); determining a starting cell for the entity (200); initiating a scan of a number of the cells from the starting cell and determining the content of each of the number of cells; and determining a total cost for the entity (200) to travel to each of the scanned cells and to perform a scan from each of the scanned cells.