Abstract: An offset module or navigation positioning estimator determines a reference frame bias between precise point positioning (PPP) reference frame and an RTK reference frame, where the PPP reference frame is associated with relative position estimates generated by the relative position estimator and where the RTK reference frame is associated RTK position estimates generated by the RTK position estimator. Upon loss of the RTK correction signal, the navigation positioning estimator or controller switches to a relative position mode based a last available RTK position. The relative position estimator determines an estimated relative position based on time-differenced phase measurements by the mobile receiver in the relative position mode. The relative position estimator or offset module offsets the estimated relative position in the relative position mode.

Abstract: A method for tracking a device not actively sending patient data to a network of medical devices is disclosed. The method comprises the device giving a signal at a time interval; an active hub listening to the device at the time interval; the active hub storing information about the device; and the active hub continuing to listen at the time interval to the device until the device actively sends patient data, or until no more signals are heard from the device. A system for tracking a device of a network of medical devices is also disclosed. The network comprises a hub and at least one device. The at least one device is configured to give a signal to the hub at a time interval, if the at least one device does not actively send patient data. The hub is configured to listen at the time interval to any devices not actively sending patient data. The hub is configured to store information about any devices not actively sending patient data.

Abstract: An apparatus and method for electromagnetic beam steering and manipulating employ narrow beams in close proximity. The beam width and distance between neighboring beams are arranged around or smaller than the wavelength. In an aspect, a strong beam is steered by a much weaker beam. In another aspect, a strong beam is focused by a small group of much weaker beams.

Abstract: Aspects of the subject disclosure may include, for example, a method for use with a communication device that includes: communicating in a first frequency band with a remote device via at least one transceiver, wherein the remote device is oriented at a direction relative to the communication device, wherein the communicating is in accordance with first antenna beam steering parameters and a first antenna beam corresponding to the direction; and, communicating in a second frequency band with the remote device via the at least one transceiver, wherein the second frequency band is higher than the first frequency band, wherein the at least one transceiver is pre-initialized with second antenna beam steering parameters to generate a second antenna beam corresponding to the direction, and wherein the second antenna beam steering parameters are generated based on the first antenna beam steering parameters.

Abstract: A hub terminal and remote client communicate via a target satellite in an inclined geosynchronous orbit. As the target satellite ascends or descends away from the geostationary arc, the signal strength of the uplink channel is increased without increasing the level of interference with adjacent geostationary satellites. The increased angular separation from adjacent satellites also decreases downlink interference. The resulting increase in signal to interference ratio permits adjustment of the modulation and coding parameters to increase spectral efficiency. The antenna gain pattern is modeled based on antenna characteristics and the model may be supplemented with measurements of a signal relayed by adjacent satellites. The method permits intermittent communication from locations where the geostationary arc is blocked or using disadvantaged antennas that would be impractical for use with geostationary satellites.

Abstract: Disclosed by way of example embodiments is a wireless communication system transmitting or receiving a wireless signal according to an orientation of the wireless communication system. In one aspect, the wireless communication system includes an antenna operable in different configurations. In each configuration, the antenna has a corresponding antenna gain in a direction with respect to the antenna. The wireless communication system further includes a sensor for determining an orientation of the wireless communication system. According to the determined orientation, the antenna is configured to transmit or receive the wireless signal in a corresponding configuration. Hence, the wireless communication system disposed in different orientations can successfully communicate with another wireless communication system.

Abstract: A method for calibrating a multichannel GNSS receiver which does not require the use of a specific signal generator and which may be implemented directly on the basis of simple measurements taken from a receiver in operation comprises determining a first, broadband equalization filter which may be positioned at the output of the RF reception channels and at the input of the correlators in order to correct the mismatch between the various RF reception channels. The invention also consists of determining a second, narrowband equalization filter in order to correct residual phase and gain errors.

Abstract: The invention relates to engineering geodesy for monitoring a height and deformation of a pipeline. The invention includes use of a complex of interrelated monitoring measures that include monitoring a control position of deformation control benchmarks using optic geodetic devices and mobile satellite geodetic receivers. A state geodetic network is used only at an initial stage for reference of the network sites to the local system of coordinates. Geodetic measurements are then converted to a local system of coordinates. The invention decreases an amount of time and labor for detection of the oil pipeline coordinates for operational needs and simplifies a planned high-altitude position data exchange, storage and transfer during measurement.

Abstract: A GPS receiver device can include at least one radio frequency (RF) chip implementing at least three RF modules configured to process RF signals received over at least three RF channels. Each RF module can be associated with a respective RF channel. Each RF module can include (1) a frequency demultiplexer and (2) at least two parallel circuits coupled to the frequency demultiplexer. Each of the parallel circuits can include (i) a RF amplifier connected to a respective output port of the frequency demultiplexer and (ii) an analog bandpass filter connected in series to the RF amplifier. The GPS receiver device can include a circuit board on which the at least one RF chip is mounted. The circuit board can have a breadth (e.g., length, width, or diameter) less than or equal to 1.65 inch.

Abstract: A method and apparatus utilizing a high-precision GNSS receiver, an EDM, and an optical camera in combination for making accurate measurements of multiple remote points. The accurate measurement of a plurality of remote points is facilitated by integrating a high-precision GNSS receiver, an EDM and an optical camera such that their combined physical location and orientation can be measured and known, and allowing for a single calibration thereof. The integration of the high-precision GNSS receiver, an EDM, and an optical camera may take various forms such as a single, integrated device, or individual devices assembled together on a surveying pole, for example. The integrated device may also include one or more sensors such as an inclination sensor and an inertial measurement unit.

Abstract: A method, user equipment (UE) and location server for estimating position of a UE based on observed angles of arrival. According to one embodiment, angles of arrival of signals from a plurality of base stations are received by a UE are observed by scanning for position reference signals (PRS) by adjusting a phase difference between antennas to cause a null of a beam of the UE to be incremented through an angular sector. For each of a plurality of base stations, an angle of arrival at which the null is steered when a PRS is suppressed by the null and a reference signal time difference, RSTD, are determined. Each angle of arrival and corresponding RSTD is transmitted to a location server which estimates UE position based on the observed angles of arrival. Further, the location server may instruct the UE to suppress a non-line-of-sight PRS signal.

Abstract: A method of generating scintillation prediction data comprises: •a) for a plurality of satellites (12A), and reference stations (10A, 10B, 10C, 10D) measuring phase scintillation data, satellite by satellite for each reference station during multiple epochs (t?2, t?1, t, t+k); •b) forecasting an expected phase scintillation value for each satellite and reference station for a period of at least 24 hours based on a cyclical prediction model; •c) for a given user location (20) and a given satellite, spatially interpolating the expected phase scintillation values of the plurality of reference stations to determine a predicted phase scintillation index; •d) repeating step c) for further satellites visible from the user location.

Abstract: A quick positioning method and a vehicle-mounted system are disclosed. The quick positioning method includes: acquiring position information from an external positioning terminal the same time when the vehicle-mounted system is started, and determining continuously whether position information is available from a local GPS positioning module; and using the position information acquired from the external positioning terminal until position information is available from the local GPS positioning module. By the above method, there would be available position information before the GPS module of the vehicle-mounted system is fully activated, thus effectively enhancing the positioning efficiency of the vehicle-mounted system.

Abstract: Disclosed is a technique that can provide one or more countermeasures against spoofers. A beamformer can control an antenna pattern of a CRPA to generate a survey beam. The survey beam is swept across space to determine a characteristic signature based on carrier-to-noise ratios (C/No) for particular space vehicle signals. Matching C/No signatures can be used to identify the existence of spoofers and invoke a countermeasure, such as nulling.

Abstract: The present invention is related to means for elimination of antenna orientation errors in millimeter wave point-to-point communication systems with beam steerable antennas. The advantage of the proposed method consists in accelerating antenna angular orientation adjustment for two connected transceivers. The advantage is achieved via determination of a value and a direction of an antenna orientation error and its further fast mechanical elimination. The method assumes transmission of radio signals and reception of them with measurement of the received signal powers. Determination of a direction and a value of an orientation error of the first transceiver antenna is achieved via measurement of the powers of signals transmitted by this antenna using different radiation patterns. Determination of a direction and a value of an orientation error of the second transceiver antenna is achieved via measurement of the powers of signals received by this antenna using different radiation patterns.

Abstract: An apparatus for indicating a direction of a radio transmission is described. The apparatus includes at least one vector detection device including two or more antennas and an attenuating material between at least one of the antennas and a source of a radio transmission. The attenuating material is arranged to vary an amount of attenuation with an angle of the source with respect to at least one of the antennas. The apparatus is configured to generate a signal indicating a direction of the radio transmission by comparing received signal strengths from the two or more antennas.

Abstract: The present disclosure provides a system and methods for mitigating, or reducing, the intermodulation of an adaptive antenna array's radiating elements. A tunable element or tunable material, such as a phase change material or a state change material, may be used to increase linearity of the RF transmission properties. These phase or state change materials may modify a radiating element's electromagnetic response. In some embodiments, variable couplers may further be added to a system to reduce intermodulation. An adaptive antenna array using the techniques described herein may have all or some of the elements co-located.

Abstract: This disclosure relates to systems and methods for verification of time sources. In various embodiments, one or more secondary time sources may be used to verify the accuracy of a primary time source prior to relying on a time signal created by the primary time source. In one embodiment, a first interface is configured to receive the primary time signal from a primary time source, and a second interface in communication with a secondary time source is configured to receive a secondary time signal. A time assessment subsystem is configured to determine an occurrence of a verification criteria. Upon the occurrence of the verification criteria, the system may compare the primary time signal and the secondary time signal to determine whether that the primary time signal is consistent with the secondary time signal. If the signal is consistent, the primary time source may be utilized by the system.

Abstract: Methods and apparatus are provided for power saving in GNSS receivers. In one novel aspect, the ME tracking period, the ME interval, and the PE working period, the PE interval are dynamically determined based on the GNSS signal conditions and/or the user requirements. In one embodiment, acceptable provision estimated position fix are used. Estimated position result is generated at each GPS position interval if there is no position result generated by the PE working period. In another embodiment, the ME-tracking and/or the PE-working are adjusted to minimum operation needs by using ME-partial (MEP) and/or PE-partial (PEP). PEP is arranged aligned with MEP. In yet another embodiment, the PE working period is delayed such that the PE working period is aligned with the ME tracking period. The position result is generated based on a last epoch's measurement obtained in the previous ME tracking period.

Abstract: Methods and systems for demodulating GNSS navigation data bits in conditions that can cause a Doppler error, such as a GNSS receiver operating under a poor clock condition, in one aspect, include: receiving a modulated Global Navigation Satellite System (GNSS) carrier signal, wherein the GNSS carrier signal includes navigation bits; compensating for a Doppler error of the GNSS carrier signal using Doppler error compensation frequencies, wherein the compensating comprises determining in-phase (I) correlation results and quadrature (Q) correlation results at the Doppler error compensation frequencies; calculating dot products using the I correlation results and the Q correlation results from the compensating; determining a dot product from the calculated dot products having a maximum absolute value; and demodulating the GNSS carrier signal using the determined dot product having the maximum absolute value to extract the navigation bits from the GNSS carrier signal.