Abstract: A method of and a system for controlling personal air vehicle (PAV) traffic provides a take-off-and-landing zone, and a forward flight zone. The take-off-and-landing zone may be from the ground up to a first altitude. The forward flight zone may be from the first altitude up to a second altitude. A maximum airspeed is provided in the take-off-and-landing zone. Minimum and maximum airspeeds are provided in the forward flight zone. In the forward flight zone there is a single heading for each altitude. Any change in heading must be accompanied by a change in altitude.

Abstract: Method and apparatus for circuit testing with ring-connected test instrument modules. A system for controlling one or more test instruments to test one or more integrated circuits includes a master clock and a controller. The test instruments are connected to form a communication ring. The master clock is connected to each test instrument and provides a clock signal to the one or more test instruments. The controller is connected to the communication ring and is configured to align counters of test instruments to derive a common clock time value from the clock signal. The controller is further configured to generate and send data words into the communication ring to carry the data words to each test instrument. The data words includes at least one data word specifying a test event to be performed, a common clock time value, and at least one of the test instruments.

Abstract: A method for reducing the turnaround time of an aircraft having at least one self-propelled undercarriage wheel comprising the step of: moving the aircraft to a required location using at least one self-propelled undercarriage wheel; wherein thrust equipment, (e.g. turbines) are turned on only when needed for takeoff or prior to landing, and are turned off until takeoff or after landing; whereby departing equipment, arriving equipment, and turnaround equipment are not at risk from operating thrust equipment, (e.g. turbines). An apparatus for reducing the turnaround time of an aircraft is disclosed comprising a control unit for facilitating voice communication between a pilot and ground staff.

Abstract: A method for managing the flow of a plurality of aircraft at an aviation resource, based upon specified data and operational goals pertaining to the aircraft and resource and the control of aircraft arrival fix times at the resource by a system manager, includes the steps of: (a) collecting and storing the specified data and operational goals, (b) processing the specified data to predict an initial arrival fix time for each of the aircraft at the resource, (c) specifying a goal function which is defined in terms of arrival fix times and whose value is a measure of how well the aircraft meet the operational goals based on achieving specified arrival fix times, (d) computing an initial value of the goal function using the predicted initial arrival fix times, (e) utilizing the goal function to identify potential arrival fix times to which the arrival fix times can be changed so as to result in the value of the goal function indicating a higher degree of attainment of the operational goals than that indicated by

Abstract: In a method for the prediction of air-traffic events, with sending means being distributed on the sites of the air-traffic actors, and with data-processing means communicating with these sending means through at least one communications network, an event is predicted by the processing means as a function of information distributed to the different sites and sent out by the sending means. The method can be applied especially to the optimizing of the management of air traffic, especially during the approach phase and in airports.

Abstract: A technique for combining a back-up aid function with a park assist function in a motor vehicle initially includes determining a distance from a motor vehicle to an object. Next, a velocity of the motor vehicle is determined. Then, a scaled version of the velocity and a minimum distance threshold are subtracted from the distance to provide a first multiplicand. Finally, a driver stimulus is provided as a function of the first multiplicand.

Abstract: Flight control indicator for an aircraft, in particular a transport airplane, intended to supply the thrust generated by at least one engine of the aircraft. The flight control indicator (1) comprises display means (4) which present, on a viewing screen (5), a dial (6) which is graduated in percentage, whose maximum represents the maximum thrust available for the current phase of flight, in the current configuration of the aircraft and for the current anemometric conditions, and which is furnished with characteristic signs (7, 8), whose positions on the dial (6) respectively represent prescribed and actual thrusts which are expressed as a percentage of the maximum thrust.

Abstract: An on-vehicle navigation system is provided with a radio wave positioning apparatus (18) and a vehicle speed sensor (13) for a dead reckoning positioning. A method of detecting a vehicle speed pulse drop of a vehicle speed pulse generated by the vehicle speed sensor is provided with: a first calculation process of calculating a first physical quantity of a predetermined type such as a velocity or the like from radio wave positioning data of the radio wave positioning apparatus; a second calculation process of calculating a second physical quantity of the same type as the first physical quantity from the vehicle speed pulse; and a detection process of detecting the vehicle speed pulse drop by using a contradiction caused between the calculated first physical quantity and the calculated second physical quantity as a detection condition.

Abstract: A method of operating a turboalternator when the turbine engine speed is between synchronous speed and self-sustaining speed.

Abstract: A vehicle traveling control system includes a control mode for controlling a vehicle speed by applying braking force so as to maintain the vehicle speed at a predetermined driving force threshold vehicle speed or smaller than that while a predetermined driving force beyond a creeping torque has been applied. The applied driving force is reduced when a target braking force required for maintaining the vehicle speed at the predetermined upper threshold vehicle speed or smaller than that is equal to a first predetermined value or greater than that. The applied driving force is increased when the target braking force or the actual braking force becomes a second predetermined value or smaller than that during the applied driving force being reduced.

Abstract: A computer program product, that allows an aviation system to temporally allocate aircraft slot times during a specified period for the flow of a plurality of aircraft toward a specified fix point, has, according to the present invention: (1) a means for collecting and storing specified data and criteria, (2) a means for processing, at a specified instant for which it is desired to allocate the slot times, the specified data applicable at that instant to each of the aircraft and associated resources so as to predict an arrival fix time for each of the aircraft at the specified fix point, (3) a means for accepting and storing a request by the operator of each of the aircraft for one of the slot times, (4) a means for accepting and storing a request by an operator of the present invention to create slack time in the specified period, (5) a means, utilizing the slot and slack time requests and the predicted arrival fix times for any of the plurality of aircraft for which a slot time request was not made, for pre

Abstract: A system for controlling a speed of a vehicle is provided. The system includes a first communications unit and a second communications unit. The first communications unit is coupled to an engine controller for controlling an engine of a first vehicle. Also, the first communications unit includes a first sending unit for sending a first message to the engine controller. The second communications unit is located remotely from the first communications unit and includes a second sending unit for sending a second message to the first communications unit to cause the first communications unit to send the first message to control the speed of the first vehicle. A method for remotely controlling the speed of a vehicle is also included which includes sending a controlling message from a remote communications unit to a proximal communications unit coupled to an engine of a vehicle.

Abstract: The invention relates to compliance with the safety distances between aircraft travelling, in a queue, one behind the other, through a prescribed air corridor. It is more especially concerned with a process allowing an aircraft knowing its position and those of the various aircraft flying in its close vicinity, for example by virtue of the ADS-B system, to manage by itself its separation distance with respect to another aircraft taken as reference. Such a process is an aid afforded to the crew of an aircraft and to the control authority regulating the traffic in the relevant air corridor.

Abstract: 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 methodology for sharing this data with the air traffic control (ATC) agency. The outcome is a daily arrival schedule providing a predetermined operational arrival time for each aircraft movement. The operational data used by the system relates to airline punctuality, taxi times at departure airfields and actual flight times predicted on a flight-by-flight basis by airline flight planning systems. This information is combined to effect a predictive arrival time at a desired navigational fix.

Abstract: The invention relates to a method and a device for assisting a driver of a vehicle, said vehicle having an engine and a braking system, an accelerator that conveys the driver's wishes concerning acceleration to the engine, and a brake pedal that conveys the driver's wishes concerneing retardation to the braking system. In accordance with the method a speed profile is determined for the driving distance, which speed profile comprises a relation between a speed set point and position. Furthermore, the engine and the braking system are controlled on the basis of the speed profile and at least one actuator influences the accelerator or braking pedal of the vehicle in accordance with said control. The driver is permitted to override the influence of the actuator only if a force that is greater than a predetermined threshold value is applied on one of the pedals.

Abstract: The instant invention provides a system and method for controlling the flight of an aircraft to meet an RTA. The system comprises a speed profile generator that communicates with a trajectory generator to produce a speed profile signal that enables the aircraft to reach a waypoint substantially at a predetermined time. In the system of the instant invention, the speed profile generator receives a nominal speed command signal, a time error signal and a sensitivity signal. Based on these inputs, the speed profile generator produces a speed profile signal. The trajectory generator receives the speed profile signal and a required time of arrival signal. Based on these signals, the trajectory generator produces a time error signal and a sensitivity signal. This sensitivity signal represents the sensitivity of the time error signal to changes in the speed profile signal.

Abstract: A system for sequencing traffic for use with various types of vehicles such as air vehicles, land vehicles water vehicles, and railroad vehicles. Virtual containers may be generated that are used to sequence traffic. The virtual containers may be suitably managed to move at a predetermined rate and capacity. Vehicles may be positioned within an empty virtual container. The vehicle will then be managed to stay within the boundaries of the virtual container and thus maintain the desired sequencing of traffic.

Abstract: 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 consideration of the surrounding weather conditions, specified data regarding the system resource and the plurality of aircraft and their operational and safety goals.

Abstract: An engine control system for a hybrid vehicle having an internal combustion engine and an electric motor as driving force sources, for permitting stopping and restarting of the engine in accordance with predetermined drive conditions. The engine control system includes a fuel cutter for cutting fuel supply to the engine when the vehicle decelerates and an engine speed detector for detecting an engine speed. Stopping of the engine is initiated by cutting the fuel supply by the fuel cutter, and when the engine speed becomes equal to or lower than a predetermined speed, the engine is stopped by operating the motor as a generator and by cutting the fuel supply.

Abstract: A method for generating a horizontal path for the avoidance of danger zones for an aircraft. The method models the contours of each danger zone by a succession of segments demarcated by points. The method determines two homing circles and two capture circles passing respectively through the initial point and final point which are tangential respectively to the initial route and to the final route and have respectively the initial and final turning radius. The method also determines tangents both to the homing circles or the capture circles and to the contour of each danger zone. Among these tangents, a pair of tangents to a homing circle and to a capture circle are selected, defining a path skeleton connecting a homing circle to a capture circle without meeting a danger zone. And, an automatically controllable evasion path that lies on the previously defined path skeleton is then determined.

Abstract: A method and associated device and management system for automatically guiding an aircraft to a parking position in a parking zone. The aircraft is detected by at least one video camera located in the parking zone which outputs video signals. The video signals are then supplied from the video camera to an evaluation unit, in which the current position of the aircraft is determined from the video signals. In addition, correction instructions for direction and speed of the aircraft are determined from the video signals in the evaluation unit. The correction instructions are transmitted to a control of the aircraft. Furthermore, in the evaluation unit, the video signals are processed into video sequences and non-aircraft objects are identified from the video signals. Finally, the correction instructions and the video sequences are displayed on a control monitor together with additional monitoring data.

Abstract: A method and a device are described for controlling a drive train of a vehicle having a gas pedal activated by a driver of the vehicle. A setpoint value is formed for a drive torque or a setpoint value for a drive power as a function of the position of a gas pedal. The drive train is then controlled in a such a way that the drive torque or the drive power is set as a function of the setpoint value formed. An interval with pre-definable interval limits is determined. The interval limits represent maximum and minimum values for the drive torque or the drive power to be set. The setpoint values are formed as a function of the determined interval. The basis for an optimal adaptation of the drive torque or the drive power to be set to the driver's preference and to the prevailing driving condition is made possible.

Abstract: Disclosed a vehicle speed control system using wireless communications, the system including a driving state detecting unit for detecting a driving state and outputting corresponding signals; a transmitter/receiver for outputting low-strength signals; an electronic control unit for receiving the signals of the transmitter/receiver and establishing an ISA mode if necessary, determining if a present driving state corresponds to a first driving state, determining if the driver has performed deceleration operations and performing control into the first driving state if needed; an engine control unit for outputting signals for control of the throttle valve opening; a throttle valve electronic control unit for outputting electrical signals to a throttle valve to control the same; and a display for displaying a present mode and a vehicle state.

Abstract: A road speed control system for preventing motorists from speeding on roads. The road speed control system includes roadside transmitter/receiver members being adapted to be erected along roadsides where speed limits on roads change; and also includes a vehicle speed control assembly being adapted to be disposed in a vehicle; and further includes a monitoring and transmitting assembly for police.

Abstract: A speed-change pattern switching control system for an automatic transmission of a motor vehicle which can ensure enhanced comfort when driving the motor vehicle. The system decides the running state of the motor vehicle on the basis of driving/operation information (Te, Tm, T&agr;, &agr;f, &agr;s), performs a first filter processing on the running state information and the driving/operation information (Vs, &thgr;, &agr;f, Ws, Ps), stores the manipulated information (Jm) for the motor vehicle in the manual speed change mode, performs a second filter processing on the manipulation information (Jm) in the manual speed change mode, outputs of the running state and the driving/operation information, and corrects speed-change patterns for the automatic transmission on the basis of output signals of the first and second filter processing.

Abstract: A system for instantaneously monitoring traffic congestion including a plurality of monitoring electronic devices located in motor vehicles traveling on roadways in a selected region. Each monitoring electronic device is coupled to a GPS receiver that provides physical location to a wireless modem capable of connecting to a wireless communication network. The system also includes a central computer connected to a wide area network that is able of continuously downloading physical location information from a plurality of monitoring electronic devices also connected to the wide area network. The central computer uses a traffic monitoring software program and a mapping database containing roadway information for a region and the movement information from the monitoring electronic devices to create a continuously updated traffic congestion database. Authorized users of the system are able to log onto the central computer to a portion of the database that contains specific traffic flow and congestion information.

Abstract: An automatic cruise control uses stored information about speeds which the vehicle used at given positions in the past to control the speed of the vehicle at a current position. In this way, the vehicle may be caused to travel at speeds in accordance with past driving history of the user. The speeds may be adjusted or overridden by the user. In addition, where a prior driving history is not available, the system can consult a database of given speeds at given locations and those speeds may be used to control the vehicular speed.

Abstract: An automatic aircraft landing system (AALS) (10) for automatically landing an aircraft on a runway. The AALS (10) includes data acquisition apparatus (DAA) (24) for acquiring flight data pertaining to the descent of an aircraft along a flight path (26) defined between a final capture point (16) and a touchdown point on the runway. The AALS (10) also includes a fuzzy logic controller (FLC) (20) responsive to the flight data for providing control signals according to at least one set of flight guidelines to at least one of the aircraft's primary controls for at least urging the aircraft to essentially adhere to a guide path (28) along at least a portion of its flight path.

Abstract: A process for managing air speed of an aircraft in flight. The method includes a first step of determining a point on the flight path at which it is theoretically possible to comply with a required time constraint by following a pre-established speed profile. In a second step, a speed is computed and a fresh speed profile is determined. This is obtained by determining speed corrections segment-by-segment from the point up to the last modifiable segment. The speed change in each segment is restricted to a maximum value. The new speed is computed on the basis of the curve showing the flight time t as a function of the speed V. This curve is approximated by a curve satisfying an equation with three coefficients (C.sub.1, C.sub.2, C.sub.3):V=c.sub.1 /t+c.sub.2 /t.sup.2 +c.sub.3 /t.sup.3Compliance with time constraints are ensured by this method while meeting the requirements of the pilot and air traffic controllers.

Abstract: A process for obtaining traffic situation data in a compressed form, while largely maintaining the reliability of the data, whereby a speed profile for a vehicle that moves in traffic and belongs to a sampling vehicle fleet ("floating car") is found and transmitted wirelessly to a traffic center from time to time. The has the following features:a) The current speed of the vehicle is found continually in the vehicle.b) In the vehicle, characterizing numbers that characterize discrete segments of the vehicle speed profile are found from the current speed values, which characterizing numbers are characteristic of the curve of the speed actually travelled in the given segment.c) The discrete segments of the speed profile are formed continuously during the vehicle trip, in that the end of a current segment, and thus the beginning of a new segment, is defined on the basis of the results of a comparison between the speed profile of the vehicle and the speed profile of at least one virtual reference vehicle.

Abstract: A digital longitudinal Aircraft Propulsion Control (APC) system of a multiengine aircraft is provided by engine thrust modulation in response to comparing an input flightpath angle signal .gamma.c from a pilot thumbwheel or an ILS system with a sensed flightpath angle .gamma. to produce an error signal .gamma.e that is then integrated (with reasonable limits) to generate a drift correction signal to be added to the error signal .gamma.e after first subtracting a lowpass filtered velocity signal Vel.sub.f for phugoid damping. The output error signal is multiplied by a constant to produce an aircraft thrust control signal ATC of suitable amplitude to drive a throttle servo for all engines, each of which includes its own full-authority digital engine control (FADEC) computer. An alternative APC system omits sensed flightpath angle feedback and instead controls the flightpath angle by feedback of the lowpass filtered velocity signal Vel.sub.f which also inherently provides phugoid damping.

Abstract: A detection device for data relating to the passage of vehicles over a road. The detection device is to be placed in a groove provided in the upper portion of the road and comprises a first profiled strip provided with an upper cavity in a U-shape, and a piezoelectric cable of the coaxial type arranged in the bottom of the cavity of the first profiled strip. A second profiled strip is arranged in the cavity of the first profiled strip on top of the coaxial cable. The second strip has a shape and dimensions such that it fills up the remaining volume of the cavity above the cable and seals this cavity.