Abstract: An integrated mobility terminal may include a modem to modulate/demodulate digital data to an intermediate frequency (IF) signal; an RF Conversion Module (RCM) to communicate between the IF signal a Radio Frequency (RF) signal for satellite communications; a Beam Forming Array (BFA) to transceive the RF signal and a Common Control Module (CCM) to manage the modem, the RCM and the BFA. The integrated mobility terminal may include a chassis to house the modem, the RCM, the BFA and the CCM, wherein the chassis is of an integrated-unitary construction.

Abstract: An integrated mobility terminal may include a modem to modulate/demodulate digital data to an intermediate frequency (IF) signal; an RF Conversion Module (RCM) to communicate between the IF signal a Radio Frequency (RF) signal for satellite communications; a Beam Forming Array (BFA) to transceive the RF signal and a Common Control Module (CCM) to manage the modem, the RCM and the BFA. The integrated mobility terminal may include a chassis to house the modem, the RCM, the BFA and the CCM, wherein the chassis is of an integrated-unitary construction.

Abstract: Power spectral density in an aeronautical satellite communication system is controlled through the use of adaptive inroute selection and spreading. Once a communication session has been established between the aircraft and the satellite, environmental conditions and aircraft conditions are monitored to detect events capable of affecting transmit/receive properties during the communication session. A maximum allowable transmission output is determined based, at least in part, on governmental regulations and the conditions being monitored. One or more transmit parameters are adjusted during the time interval in order to maintain transmission output power of the aircraft terminal below the maximum allowable transmission output power.

Abstract: Power spectral density in an aeronautical satellite communication system is controlled through the use of adaptive inroute selection and spreading. Once a communication session has been established between the aircraft and the satellite, environmental conditions and aircraft conditions are monitored to detect events capable of affecting transmit/receive properties during the communication session. A maximum allowable transmission output is determined based, at least in part, on governmental regulations and the conditions being monitored. One or more transmit parameters are adjusted during the time interval in order to maintain transmission output power of the aircraft terminal below the maximum allowable transmission output power.

Abstract: Power spectral density in an aeronautical satellite communication system is controlled through the use of adaptive inroute selection and spreading. Once a communication session has been established between the aircraft and the satellite, environmental conditions and aircraft conditions are monitored to detect events capable of affecting transmit/receive properties during the communication session. A maximum allowable transmission output is determined based, at least in part, on governmental regulations and the conditions being monitored. One or more transmit parameters are adjusted in order to maintain transmission output power of the aircraft terminal below the maximum allowable transmission output power.

Abstract: It is determined, e.g., in a communications terminal, that a test triggering event has occurred. A test is initiated based on the determination that the test triggering event has occurred. One or more transmissions are transmitted at one or more respective specified power levels. Measurement data is received from a remote measurement unit indicating respective received power levels of the one or more transmissions by the remote measurement unit. Based on the measurement data, a maximum transmit power level is determined.

Abstract: A mobile terminal for satellite communications receives communication, e.g., from a gateway via a satellite link. A frequency lock loop unit locks to the carrier frequency of the received communication. The mobile terminal includes a global positioning system for receiving global positioning data. The mobile terminal determines the Doppler frequency shift of the received communications based on the global positioning data. The mobile terminal generates a reference clock for return transmissions based on the frequency of the frequency lock loop, corrected for the Doppler shift. A correction factor of two times the determined Doppler frequency shift is used, to compensate for both a forward and return transmission link.

Abstract: It is determined, e.g., in a communications terminal, that a test triggering event has occurred. A test is initiated based on the determination that the test triggering event has occurred. One or more transmissions are transmitted at one or more respective specified power levels. Measurement data is received from a remote measurement unit indicating respective received power levels of the one or more transmissions by the remote measurement unit. Based on the measurement data, a maximum transmit power level is determined.

Abstract: A telecommunications system includes a network device that receives a data signal over a first communication network and in accordance with a first communication protocol. The network device generates an acknowledgement command for a remote device to transmit an acknowledgement signal over a second communication network and in accordance with a second communication protocol. The acknowledgement signal acknowledges receipt of the data signal at the network device.

Abstract: A mobile terminal for satellite communications receives communication, e.g., from a gateway via a satellite link. A frequency lock loop unit locks to the carrier frequency of the received communication. The mobile terminal includes a global positioning system for receiving global positioning data. The mobile terminal determines the Doppler frequency shift of the received communications based on the global positioning data. The mobile terminal generates a reference clock for return transmissions based on the frequency of the frequency lock loop, corrected for the Doppler shift. A correction factor of two times the determined Doppler frequency shift is used, to compensate for both a forward and return transmission link.

Abstract: A small vehicle detector for determining a size of a vehicle entering a particular area and assigning a rate of charge based on the determined size of vehicle including an entrance for a vehicle to enter the area. The small vehicle detector further includes a vehicle size detector system for determining size of the vehicle. The small vehicle detector also includes a ticket dispenser for dispensing a ticket with the assigned rate of charge based on the size determined by the vehicle size detector.

Abstract: A small vehicle detector for determining a size of a vehicle entering a particular area and assigning a rate of charge based on the determined size of vehicle including an entrance for a vehicle to enter the area. The small vehicle detector further includes a vehicle size detector system for determining size of the vehicle. The small vehicle detector also includes a ticket dispenser for dispensing a ticket with the assigned rate of charge based on the size determined by the vehicle size detector.

Abstract: A small vehicle detector for determining a size of a vehicle entering a particular area and assigning a rate of charge based on the determined size of vehicle including an entrance for a vehicle to enter the area. The small vehicle detector further includes a vehicle size detector system for determining size of the vehicle. The small vehicle detector also includes a ticket dispenser for dispensing a ticket with the assigned rate of charge based on the size determined by the vehicle size detector.

Abstract: A small vehicle detector for determining a size of a vehicle entering a particular area and assigning a rate of charge based on the determined size of vehicle including an entrance for a vehicle to enter the area. The small vehicle detector further includes a vehicle size detector system for determining size of the vehicle. The small vehicle detector also includes a ticket dispenser for dispensing a ticket with the assigned rate of charge based on the size determined by the vehicle size detector.

Abstract: The invention relates to a sliding surface (1), which is applied by arc spraying with the aid of a rotating tool. During the spraying process, the parameters are to be set in such a way that all the material particles are fused. The benefit of the high degree of fusion is that the sliding surface (1) can be machined by precision turning without the uncontrolled eruption of material. The rotating spraying process orientates the surface roughness on the face (1.2) of the sliding surface (1) transversally in the peripheral direction. This enables valley structures in the form of recesses (1.1) to be produced during the precision turning process, said recesses having a Peklenit factor of less than 1, achieving a high degree of flow obstruction and forming a defined oil-retaining volume.

Abstract: A satellite-based communications network employing at least one satellite and a plurality of user terminals adapted for use with the communications network. The network includes a transmitter for transmitting data to the plurality of user terminals, where the data includes a plurality of broadcast modes and/or services. The transmitter transmits data in a packetized format in which a predetermined number of data packets are transmitted in a frame, where the frame is defined as a predetermined period of time. Further, the transmitter transmits each of the plurality of broadcast modes utilizing a single carrier frequency. Each of the plurality of user terminals includes a receiver for receiving the transmitted data and for regenerating the data so that the data is made available to a device coupled to the user terminal.

Abstract: A method of pointing an antenna at a transmitter comprising the steps of: (a) varying the azimuth of the antenna dish a predetermined number of degrees in a first direction from a predetermined azimuth angle; (b) measuring a first signal strength of an incoming signal received by the antenna dish; (c) varying the azimuth of the antenna dish the same predetermined number of degrees in a second direction from the predetermined azimuth angle, where the second direction is opposite to the first direction; (d) measuring a second signal strength of the incoming signal received by the antenna dish; and (e) comparing the first signal strength to the second signal strength, and if the first signal strength substantially equals the second signal strength, the current predetermined azimuth angle represents the optimal angle of azimuth for the antenna dish.

Abstract: A method of printing a substrate includes contact printing a first graphic in a first operation and non-contact printing a second graphic in a second operation. A method of printing an outer cover for an absorbent article includes contact printing the outer cover in a first operation, non-contact printing the outer cover in a second operation, and joining the outer cover with an absorbent and a liner to produce an absorbent article. A method of minimizing substrate printing waste includes contact printing absence advertisements in a first operation and non-contact overprinting a second graphic in a second operation. A method of distributing customized products to different customers includes contact printing substantially uniform graphics on a substrate in a first operation, non-contact printing customized graphics on a substrate in a second operation, and distributing the substrate to customers.

Abstract: The present invention relates to a method and apparatus of using ephemeris data for positioning of an antenna of an earth station. Ephemeris data is transmitted from the satellite to the earth station, wherein the ephemeris data comprises positioning data of a satellite. The ephemeris data is received by the earth station and is used to realize the location of the satellite. The antenna of the earth station is adjusted to point toward the satellite, using the received ephemeris data.

Abstract: An antenna of an earth station is adjusted at a predetermined interval for calibration purposes. A notification of clear sky is received. Signals from a satellite are received upon the receiving of the notification of clear sky. The antenna of the earth station is adjusted to point in various directions while receiving the signals from the satellite. A direction is determined where the antenna of the earth station is pointing where the strongest signal is received from the satellite. The antenna of the earth station is positioned to point in the direction where the strongest signal is received by the satellite.