JP2011257418A - Satellite positioning support - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide an easy operation of satellite signal measurement.SOLUTION: A satellite signal receiver 40 includes a measurement component 43 that measures a received satellite signal. The receiver further includes a first processing unit 44 so as to improve the operability of the measurement, and the first processing unit 44 executes a software 45 that controls the measurement component 43 based on a received control parameter. The receiver also includes a first interface component 46 that receives a control parameter from an another processing unit 35 through an another interface component 34, supplies the control parameter to the first processing unit 44, and transmits the measurement result obtained from the measurement component 43 to the another processing unit 35 through the another interface component 34.

Description

  The present invention relates to a satellite signal receiver, and more particularly to a mobile device that supports positioning by a satellite. The invention also relates to a method for supporting positioning by satellite. The invention further relates to an interface and software code for a mobile device that supports satellite positioning.

  Currently, GPS (Global Positioning System) is an American system and GLONASS (Global Orbiting Navigation Satellite System) is a Russian system. There are two). In the future, another European system called GALILEO will emerge. The general term for these systems is GNSS (Global Navigation Satellite System).

  For example, for GPS, more than 20 satellites are in orbit around the earth. Each satellite transmits two carrier signals L1 and L2. One of these carrier signals, L1, is employed to carry standard positioning service (SPS) navigation messages and code signals. The phase of the L1 carrier is modulated by each satellite using a separate C / A (Coarse Acquisition) code. Thus, different channels are acquired for transmission from different satellites. The C / A code is a pseudo random noise (PRN) code that spreads the spectrum over a nominal bandwidth of 20.46 MHz. The C / A code is repeated every 1023 bits, and the epoch of this code is 1 millisecond. The bit of the C / A code is also referred to as a chip. Furthermore, the carrier frequency of the L1 signal is modulated using navigation information with a bit rate of 50 bits per second. Specifically, the navigation information includes a time stamp indicating a transmission time and an ephemeris parameter. The orbital calendar parameter describes a small section of the orbit of each satellite. Using the algorithm based on the above orbital calendar parameters, the position of the satellite at an arbitrary time can be estimated while the satellite is in each described section.

  A GPS receiver that is subject to position calculation receives a signal transmitted from a currently available satellite, and a communication path used by each satellite based on each C / A code included in the signal Detect and track. In order to capture and track the satellite signal, the signal received at the radio frequency (RF) portion of the GPS receiver is first converted to baseband. In the baseband portion, for example, a frequency error caused by the Doppler effect is removed by the mixer. The signal is then correlated with the replica code obtained for each satellite. The correlation can be taken using a matched filter, for example. Furthermore, correlation values can be integrated coherently and / or incoherently to improve the sensitivity of acquisition. If the correlation value exceeds the threshold value, it can be seen that there is a C / A code and its code phase, which are necessary for spreading the signal and thus for restoring the navigation information.

  Next, the receiver generally calculates the transmission time of the code transmitted from each satellite based on the data of the encoded navigation message and the number of epochs and chips of the C / A code. From the transmission time and the measured arrival time of the signal at the receiver, the propagation time required for the signal to propagate from the satellite to the receiver can be calculated. When this propagation time is multiplied by the speed of light, it can be converted into a distance or range between the receiver and each satellite.

  Since the receiver is located at the intersection of the range from a set of satellites, the current position of the receiver can be calculated from the calculated distance and the estimated satellite position.

  Similarly, the general concept of GNSS positioning is that the time taken for the signal to propagate from the estimated satellite position to the receiver by receiving the satellite signal at the receiver to be positioned. To measure and thereby calculate the distance between the receiver and each satellite, as well as the current position of the receiver, further utilizing the estimated position of the satellite.

  GPS positioning can be performed in three different positioning modes. The first mode is positioning using self-supporting GPS. This means that when a GPS receiver receives signals from GPS satellites, it calculates the position from these signals without obtaining any additional information from another source. The second mode is GPS (AGPS) positioning using a network-assisted mobile device. In this mode, the GPS receiver may be associated with the mobile communication device. The GPS receiver may be integrated into the mobile communication device or may be an accessory of the mobile communication device. Assistance data provided by the mobile communication network is received by the mobile communication device and transmitted to the GPS receiver to improve its performance. Such support data includes at least ephemeris, position and time information, and the like. In this case, the positioning calculation is performed in the GPS receiver. The third mode is GPS positioning supported by a mobile device using a network. In this mode as well, the GPS receiver is associated with the mobile communication device. In this mode, the mobile communication network supplies at least acquisition assistance and time information to the GPS receiver via the mobile communication device to assist in the measurement. Next, the measurement result is supplied to the mobile communication network via the mobile communication device, and the mobile communication network calculates the position. The second and third methods are commonly referred to as assisted GPS (AGPS).

  Since the receiver has to process different information in different modes, conventional receivers only support one of the above modes or switch between these modes. It corresponds.

  Conventional GPS receivers for positioning using self-supporting GPS or for positioning using support self-supporting GPS use a single functional entity to perform measurements, control measurements, and perform positioning calculations. I have. At least part of the measurement execution is performed using hardware, and at the same time, at least part of the measurement control and positioning calculation is realized in software. This situation is illustrated in FIG. 1, which is a schematic block diagram of a satellite positioning system.

  The system comprises a mobile phone 10, a GPS satellite 11, and a base station 12 of a GSM network or any other cellular network. The mobile phone 10 includes a GPS receiver 13. The GPS receiver 13 includes an RF component 14 and a measurement and positioning component 15. The RF component 14 and the measurement and positioning component 15 can be implemented, for example, on separate chips or on a single chip. The mobile phone 10 further comprises a cellular engine 16, i.e. a module with all the components necessary for conventional mobile communication between the mobile phone 10 and the mobile communication network. Furthermore, the cellular engine 16 executes conversion software 17 that is adapted to convert assistance data supplied by the base station 12 for use by the GPS receiver 13.

  Support data protocols between the cellular engine 16 and various types of communication networks are being standardized and are already in use. Specifically, a radio resource location service protocol (RRLP) is used in a network using a global system for mobile communications (GSM), and radio resource control (RRC: Radio Resource Control (protocol) is used in networks using wideband code division multiple access (WCDMA), and IS-801 protocol uses code division multiple access (CDMA). Used in the network. These protocols typically do not support a unique interface between the cellular engine 16 and the GPS receiver 13. Instead, the cellular engine 16 must have software 17 that converts the data supplied by the network protocol into an appropriate format.

  More specifically, each GPS hardware supplier has so far defined a unique interface for the interface between the GPS receiver 13 and the cellular engine 16. In general, these interfaces use the standard National Marine Electronics Association (NMEA) protocol for autonomous GPS functionality and / or access more detailed information about GPS receivers. Use a message specific to the supplier and / or use a specific message to supply assistance data from the network to the GPS receiver for AGPS functionality. Specific formats for such suppliers include, for example, Texas Instruments (registered trademark) cellular modem interface, Motorola (registered trademark) GPS interface, and the like.

  U.S. Pat. No. 6,542,823 (B2) describes a server that reciprocates between a call processor and a GPS client to transmit data.

  WO 2004/107092 (A1) describes the use of a conversion mechanism at the interface between a mobile device call processor and the mobile device GPS module. The conversion mechanism converts the protocol used to provide assistance data to the mobile device into a proprietary protocol used by the GPS module.

  With conventional GPS receivers, it is difficult to evaluate the exact performance of GPS measurement hardware. Similarly, it is difficult to exchange from one GPS measurement hardware to another without extensive work in software. Furthermore, it is difficult to implement a hybrid positioning solution using cellular network measurement data or motion sensor data.

  The present invention facilitates the operation of satellite signal measurement.

  A satellite signal receiver that supports positioning by satellite is proposed. The satellite signal receiver includes a measurement component adapted to perform measurement of the received satellite signal and a first processing unit adapted to execute software for controlling the measurement component based on the received control parameter. And. The satellite signal receiver further comprises a first interface component, which receives control parameters from another processing unit via another interface component and supplies the control parameters to the first processing unit. The measurement result obtained from the measurement component is transmitted to another processing unit via another interface component.

  Further, a mobile device that supports positioning by satellite is proposed. The mobile device comprises the satellite signal receiver proposed above. In addition, the mobile device comprises another processing unit. The other processing unit is adapted to execute control software for generating control parameters for the measurement component and evaluation software for processing the measurement result supplied from the measurement component. The mobile device further comprises another interface component. The other interface component forwards the control parameters generated by the other processing unit to the first interface component and sends the measurement results received from the first interface component to the other processing unit. It has become.

  In addition, an interface for a mobile device that supports satellite positioning is proposed. Assume that the mobile device comprises a satellite signal receiver having a measurement component and a first processing unit. Assume that the mobile device further comprises another processing unit. The interface proposed above is configured to allow communication between the satellite signal receiver and another processing unit. The interface comprises a first interface component in the satellite signal receiver and another interface component. The first interface component receives control parameters from another interface component, supplies control parameters to the first processing unit, and sends measurement results obtained from the measurement component to the other interface component. ing. The other interface component transfers control parameters generated by the other processing unit to the first interface component, and transmits the measurement results received from the first interface component to the other processing unit. ing.

  Furthermore, a method for supporting positioning by a satellite in a mobile device is proposed. This mobile device is based on the same assumptions as for the interface proposed above. The proposed method includes generating control parameters for the satellite signal receiver in another processing unit and transferring the control parameters to the satellite signal receiver via the interface. The proposed method further includes controlling the measurement of the received satellite signal by the measurement component based on the transferred control parameters at the satellite signal receiver using the first processing unit. The proposed method further includes the step of transferring the measurement result of the measurement component to another processing unit via the interface. The proposed method further comprises the step of processing the transferred measurement results in another processing unit.

  Furthermore, a first software code for a mobile device that supports positioning by satellite is proposed. This mobile device is based on the same assumptions as for the interface proposed above. When operating in another processing unit, the first software code generates a control parameter for the satellite signal receiver so that the control parameter is transferred to the satellite signal receiver via the interface. Furthermore, the first software code processes the measurement results received from the satellite signal receiver via the interface. Similarly, a software program product storing such software code is proposed.

  In addition, a second software code for a mobile device that supports satellite positioning is proposed. This mobile device is based on the same assumptions as for the interface proposed above. When operating in the first processing unit, the second software code controls the measurement of the received satellite signal by the measurement component based on control parameters supplied via the interface from another processing unit. Furthermore, the second software code causes the measurement result of the measurement component to be transferred to another processing unit via the interface. Similarly, a software program product storing such software code is proposed.

  The present invention is based on the concept that if the control parameter generation and positioning functions are removed from the satellite signal receiver, the measurement functions of the satellite signal receiver can be utilized in a more flexible manner. It is therefore proposed to implement instead the control parameter generation function and the measurement value processing function in software executed by an independent processing unit. The necessary communication between the satellite signal receiver and the independent processing unit takes place via a new interface. This interface is adapted to provide low level information in the form of control parameters required for the measurement of received satellite signals. The term “low level” relates to any aspect involving real-time acquisition and tracking of satellite signals by measurement components.

  As an advantage of the present invention, the performance evaluation and inspection of the measurement components of a satellite signal receiver can be simplified. Further, by entrusting processing to the outside, the satellite signal receiver itself is simplified, thereby reducing the cost of the satellite signal receiver. In addition, the present invention supports the development of satellite positioning solutions and reduces the software work required for such solutions. For example, in a mobile device according to the present invention, it can be freely replaced with any measurement component compatible with the interface employing the measurement component, whereas in a conventional receiver, Because the software and baseband measurement components are tightly integrated, it is not possible to replace the software without adjustment.

  The satellite signal receiver can be realized in various ways. For example, it may be a discrete chip with a radio frequency (RF) portion and a baseband portion in the same package. Further, it may be a chip set including the RF portion and the baseband portion in different packages. Furthermore, it may be integrated with another component of the mobile device, for example with the cellular engine of the mobile communication device. Similarly, it may be partly integrated with another component and partly mounted on an independent chip. For example, the RF portion can be integrated and the baseband measurement portion can be mounted on a separate chip.

  The measurement component may specifically perform only the baseband processing of the received signal including all measurements performed in the baseband, but similarly it may execute any processing in the RF domain, for example. May be. The measurement component can be realized in hardware. Alternatively, some may be implemented in hardware and some may be implemented in software, as in the case of a “snapshot GPS” receiver or a “software GPS” receiver. The measurement component using hardware and software may comprise, for example, a memory for storing samples of received satellite signals, a processor for processing sampled and stored satellite signals, and the like. More specific processing can be performed by low-level software and logic for signal acquisition, signal tracking, signal verification and data reception.

  In one embodiment of the invention, the measurement component is adapted to perform measurements of received satellite signals transmitted from satellites of at least two different satellite positioning systems, which are software executed by the first processing unit. That is, depending on the control parameters supplied by the other processing unit. The measurement component may be adapted to measure, for example, a GPS signal, a GALILEO signal, a GLONASS signal, or any combination thereof.

  The software executed by the first processing unit and controlling the measurement component based on the control parameters supplied from the other processing unit may also be low level software. This software can be used, for example, for power saving settings, frequency calibration, time calibration, automatic gain control (AGC) tuning, pulse per second (pps) generation, and / or measurement interval settings. concern. The above task is also executed in a conventional satellite signal receiver. However, according to the present invention, unlike the conventional satellite signal receiver, control data that is the basis of control is generated externally. The

  In an embodiment of the present invention, the first processing unit executes software to convert the measurement result of the measurement component into a format suitable for position information calculation in the other processing unit.

  In one embodiment of the present invention, the first processing unit can be flexibly used for at least two positioning modes, for example, for self-supporting positioning, network-assisted positioning, and network-based positioning. be able to. In any case, the function of the first processing unit may be essentially the same regardless of the positioning mode, i.e. the same method can be used for every positioning mode, so that this satellite signal receiver May be modeless. This is possible because in the network support mode and the network use mode, the first processing unit does not need to evaluate the received support information and generate necessary control parameters, and directly in any mode. This is because control parameters that can be implemented are received.

  Also in the mobile device, the processing of the measurement results performed by the other processing unit is substantially the same for all corresponding positioning modes. This means that even if the positioning mode is based on a network, information related to positioning can be calculated in the mobile device. This requires higher processing power than simply transmitting measurement results, but at the same time can improve performance in certain situations. For example, when a position is calculated in a terminal for a tracking application based on a network, tracking performance and sensitivity are superior to that of a positioning calculation on a network, and power consumption is reduced.

  A control parameter is a parameter that can be used directly to control a measurement component without any additional calculations. At best, format conversion is necessary. Advantageously, the control software executed by the other processing component is adapted to generate control parameters for the measurement component from a format suitable for the satellite signal receiver.

  There may be various types of control parameters. The control parameter includes, for example, a predicted signal characteristic such as a predicted code phase at a specific time with 1 sigma uncertainty and a prediction such as a predicted Doppler frequency at a specific time with 1 sigma uncertainty. Doppler effect, other predicted uncertainties, timing information, reference frequency quality, etc. may be included. The control parameters may further include various mode parameters such as a communication path reset request, a power saving mode, and a tracking mode.

  The control parameters can be generated, for example, completely in the mobile device. Furthermore, for example, the support data that can be obtained can be generated by converting the data into a protocol-independent format.

  Thus, the proposed architecture can remove all associations to protocols and standards, such as cellular standards, from which assistance data is supplied, from the receiver hardware.

  The control software executed by the other processing unit is also involved in generating the necessary response messages for the entity supplying assistance data according to a corresponding protocol such as NMEA or RRLP. Good.

  Of course, the evaluation software executed by another processing unit may also take into account information other than satellite signal measurements when processing the measurement results for the purpose of position information calculation.

  Further, this interface may be similarly adopted for other types of message communication other than GPS message communication. In one embodiment according to the present invention, the first interface component is further adapted to transmit positioning results not related to satellite positioning from the measuring component to another interface component. Next, another interface component may transmit the above measurement result received from the first interface component to another processing unit. Such supplementary measurement results include, for example, sensor measurement, temperature measurement, atmospheric pressure measurement, acceleration measurement, compass direction measurement results, and the like.

  In one embodiment according to the invention, the proposed mobile device consists of a mobile communication device such as a mobile phone, for example. In this case, the control software and the evaluation software may be implemented in software that supports communication of the mobile communication device via the mobile communication network. Examples of the software include an intelligent software architecture (ISA) by Nokia (registered trademark), a Symbian (registered trademark) application, and a Java (registered trademark) application.

  If the mobile device comprises a mobile communication device, the mobile device may be a mobile communication device incorporating a satellite signal receiver. Alternatively, the satellite signal receiver may be an accessory device of the mobile communication device.

  In one embodiment according to the invention, the first interface component and the other interface component are adapted to use a dedicated protocol for exchanging control parameters and measurement results. This protocol may define a non-real-time interface, i.e. independent of cellular standards, independent of satellite signal receiver hardware, specifically measurement hardware, and yet another positioning Allows the unit to work with any satellite signal receiver that supports the interface.

  The interface can in particular employ a low level hardware connection between interface components, such as a universal asynchronous receiver and transmitter (UART) connection, a serial peripheral interface (SPI). Interface (Inter-Integrated Circuit bus) connection, Bluetooth (registered trademark) connection, ultra wide band (UWB) connection, or infrared (IR) connection It is done.

  The present invention can be employed in any mobile device that can receive satellite signals. Of course, the present invention is equally applicable with satellite augmentation systems such as the Wide Area Augmentation System (WAAS) and European Geostationary Navigation Overlay System (EGNOS). be able to. WAAS and EGNOS calculate GPS correction data taking into account GPS signal delays caused by the atmosphere and ionosphere. Correction data transmitted via geostationary satellites can be received by a suitable GPS receiver and used to improve the accuracy of GPS-based positioning.

  Other objects and features of the present invention will become apparent from the following detailed description considered in conjunction with the accompanying drawings.

It is a schematic block diagram of the conventional assist GPS system. 1 is a schematic block diagram of a satellite positioning system according to an embodiment of the present invention. It is a schematic block diagram which shows the detail of the system of FIG. 4 is a flowchart showing operations in the system of FIGS. 2 and 3.

  FIG. 2 is a schematic block diagram of a satellite positioning system in which the functions of the satellite signal receiver are divided according to the present invention.

  The system includes a mobile phone 20, a satellite 21 and a network element 22.

  The mobile phone 20 is an exemplary configuration according to the present invention. It includes a cellular engine 30, that is, a module that includes all the components necessary for conventional mobile communication between the mobile phone 20 and the mobile communication network. The cellular phone 20 further includes a satellite signal receiver 40. The satellite signal receiver 40 includes a conventional RF component 41. However, unlike conventional satellite signal receivers, the measurement and positioning component 15 is not included, but only the measurement module 42 is provided. An independent positioning module 31 is mounted on the cellular engine 30. The measurement module 42 and the positioning module 31 are connected to each other by an interface (I / F) 50. The satellite signal receiver 40 may be realized in the form of a chip, on which the RF component 41 and the measurement module 42 may be mounted.

  The satellite 21 is one of a plurality of satellites that are in the orbit of the earth and transmit a code-modulated signal to enable positioning by the satellite. The satellite 21 can be a GPS satellite, a GALILEO satellite, a GLONASS satellite, or the like.

  The network element 22 can be, for example, a base station of a GSM network. If necessary, the network element 22 can supply satellite positioning support data to the mobile phone.

  Details of the cellular engine 30 and satellite signal receiver 40 are shown in FIG.

  As already shown in FIG. 2, the satellite receiver 40 comprises an RF component 41 and a measurement module 42. The measurement module 42 is adapted to measure signals transmitted from GPS satellites, GLONASS satellites, GALILEO satellites, and combinations thereof.

  The measurement module 42 comprises an actual measurement component 43 and a digital signal processor (DSP) 44 as a first processing unit for performing measurements. The DSP 44 is adapted to execute a control and data exchange component 45 that is low-level software that controls the measurement component 43.

  The measurement module 42 further includes an I / F component 46 as a first interface component, which interacts with the control and data exchange component 45.

  As an example, the measurement component 43 may be a pure baseband measurement component that performs measurements at baseband, but at the same time may additionally perform RF measurements, or the RF component 41 may be fully It can also be included. This can only be realized in hardware controlled by the control and data exchange component 45. Alternatively, the measurement component may comprise a memory for satellite signal samples and a processor for processing the sampled and stored satellite signals. In the latter case, it will be appreciated that this processor may correspond to a DSP 44 executing appropriate measurement software. In either case, measurement component 43 is responsible for performing signal acquisition, signal tracking, code and carrier phase measurement, signal verification, and navigation data reception based on satellite signals received by RF component 41. .

  The measurement module 42 is modeless, that is, its function is exactly the same regardless of a selected positioning method such as a self-supporting positioning method, a network-assisted positioning method, or a network-based positioning method.

  The cellular engine 30 includes several components, and in particular, includes a DSP 35 as another processing unit. The DSP 35 is adapted to execute cellular engine software, that is, software that supports communication with the mobile communication network. This software may be, for example, ISA software or Symbian® software. The positioning module 31 is realized in software implemented in the cellular engine software and can therefore be executed by the DSP 35 as well. The positioning module 31 includes an evaluation component 32 adapted to perform positioning calculation and the like. The positioning module 31 further comprises a control component 33, which collects information for measurements performed by the satellite signal receiver 40.

  The cellular engine 30 further includes an I / F component 34 as another interface component, which interacts with both the evaluation component 32 and the control component 33.

  I / F component 34, I / F component 46, and the physical low level connection between these components form interface I / F 50, thereby exchanging data between satellite signal receiver 40 and positioning module 31. Is possible. The above connection may be a UART connection, for example. The I / F component 34 and the I / F component 46 correspond to the selected connection technology using a dedicated protocol.

  Here, the operation of the system of FIGS. 2 and 3 will be described in more detail with reference to the flowchart of FIG.

  When positioning of the mobile phone 20 is performed, the control component 33 generates control parameters for the satellite signal receiver 40. The control component 33 generates a low level parameter that indicates whether the measurement module 42 should capture GPS, GLONASS and / or GALILEO signals. Included here are indicators such as predicted signal code phase, predicted Doppler frequency, predicted code and Doppler uncertainty, reference frequency details, and reference time details. The control component 33 further generates low level control parameters to place the measurement module 42 in a particular state. For example, there are a power saving state, a power-off state, a power-on state, and a self-test state. The generated control parameters are in a default “satellite positioning system type” that can be used by the control and data exchange component 45 (step 411).

  In addition, the control component 33 may convert the available assistance data into a format suitable for the measurement module 42. The assistance data may be supplied to the control component 33, for example by the network element 22 of the mobile communication network, or by another source, for example a wireless local area network (WLAN) or from a memory. The assistance data may include, for example, information related to the reference position, so that the search for capturing the satellite signal can be limited. In order to convert the assistance data into an appropriate format, the control component 33 removes the dependency of the assistance data protocol and converts the assistance data into the “satellite positioning system format”. Control component 33 also generates the necessary response message for the entity supplying the assistance data using the required protocol, such as RRLP (step 412).

  The I / F component 34 converts the generated control and support data into the measurement module 42 using the implemented connection technology, and thus the I / F format preset for the generated control and support data. Transfer to the I / F component 46 (step 413).

  The I / F component 46 of the measurement module 42 receives the control and support data in the I / F format, restores the control and support data to the original “satellite positioning system format”, and transfers the control and support data to the control and data. Supply to the replacement component 45 (step 421).

  The control and data exchange component 45 controls the operation of the measurement component 43 according to the setting parameters supplied from the control component 33. More specifically, the data exchange component 45 produces a corresponding frequency calibration, corresponding time calibration, corresponding AGC tuning, corresponding pps generation, corresponding signal acquisition, corresponding signal tracking, corresponding measurement data response. What is necessary is just to obtain | require each measurement interval. In addition, it seeks to save power based on the control data. The measurement component 43 supplies measurement results to the control and data exchange component 45. The measurement result may include, for example, identification information of the satellite from which the captured signal is transmitted, the reception time of the captured satellite signal, decoded navigation information, and the like (step 422).

  The control and data exchange component 45 converts the measurement result to a low-level “position calculation format” suitable for performing the positioning calculation in the positioning module 31 (step 423).

  The I / F component 46 uses the connected connection technology, and hence the I / F format preset for the converted measurement result, to convert the converted measurement result into the I / F component 34 of the cellular engine 30. (Step 424).

  The I / F component 34 of the cellular engine 30 receives the converted measurement result in the I / F format, restores the converted measurement result to the original “position calculation format”, and evaluates the converted measurement result as an evaluation component. (Step 414).

  The evaluation component 32 calculates position information based on the measurement result, and includes, for example, calculation of the current position of the mobile phone 20, calculation of the current speed of the mobile phone 20, and calculation of the current time. It is. The evaluation component 32 receives supplementary information that supports the calculation of position information, for example, measurement values relating to signals exchanged with the network element 22 of the mobile communication network, or ephemeris data supplied from the network element 22. (Step 415).

  The result of the location information calculation may then be presented to the user or used as input data for some application such as a navigation application (step 416).

  It should be noted that the described embodiment is merely one of various possible embodiments of the present invention.

Claims (21)

A device,
A measurement component configured to perform measurements on received satellite signals;
A first processor and software code, wherein the processor is configured to control the measurement component based on received control parameters using the software code;
A first interface component configured to receive control parameters from another processor external to the device via another interface component and supplying the control parameters to the first processor A first interface component configured to:
The first processor is further configured to convert the measurement result of the measurement component into a format suitable for position information calculation in the other processor using the software code,
The apparatus, wherein the first interface component is further configured to send the converted measurement result to the another processor via the another interface component.   The measurement component is configured to perform a measurement on a received satellite signal in response to a control parameter provided by the another processor, the control parameter being a received satellite of at least two different satellite positioning systems. The apparatus of claim 1, comprising instructions for a system that performs signal measurements.   The apparatus of claim 1, wherein the first interface component is configured to employ a dedicated protocol for receiving control data and transmitting measurement results.   The first processor uses the software code to control the measurement component to provide measurement results for at least two of positioning modes of self-supporting positioning, network-assisted positioning, and network-based positioning. The apparatus of claim 1, configured as follows.   The apparatus of claim 4, wherein the first processor is configured to use the software code to control the positioning component in essentially the same manner for each of the at least two positioning modes. A mobile device that supports satellite positioning,
An apparatus according to claim 1;
Said another processor configured to generate control parameters for said measurement component using control software and converted to an appropriate format supplied by said measurement component using evaluation software Said another processor configured to process the measured result,
A control parameter generated by the another processor, transferred to the first interface component, and a measurement result received from the first interface component is transferred to the other processor; Said another interface component configured to transmit; and
A mobile device comprising:   7. The further processor is configured to generate control parameters for the measurement component in a format suitable for the apparatus of claim 1 using the control software. The mobile device described.   The another processor uses the control software to convert control data for the measurement component by converting available assistance data into a protocol-independent format suitable for the apparatus of claim 1. The mobile device of claim 7, configured to generate.   The first interface component is further configured to transmit measurement results from the measurement component not related to satellite positioning to the other interface component, wherein the other interface component is configured to transmit the first interface component to the first interface component. The mobile device according to claim 6, wherein the mobile device is configured to transmit the measurement result received from an interface component to the another processor.   The first processor and the other processor are configured to correspond to at least two of positioning modes of self-supporting positioning, network-assisted positioning, and network-based positioning, and the first processor , Configured to control the measurement component in essentially the same manner for each of the at least two positioning modes, wherein the another processor is essentially the same method for each of the at least two positioning modes. The mobile device according to claim 6, wherein the mobile device is configured to execute the processing of the measurement result.   The mobile device includes a mobile communication device, and the control software and the evaluation software are realized by software configured to support communication of the mobile communication device via a mobile communication network. The mobile device according to claim 6.   The mobile device according to claim 6, wherein the mobile device is a mobile communication device.   The mobile device comprises a mobile communication device that includes the another processor and the other interface component, and the device of claim 1 is an accessory device of the mobile communication device. The mobile device according to claim 6. Software code for a mobile device supporting positioning by a satellite, wherein the mobile device comprises a satellite signal receiver including a measurement component and a first processor, and the mobile device comprises another processor. , When the software code is running in the first processor, the satellite signal receiver has the following steps:
Receiving control parameters from said another processor via an interface;
Controlling the measurement of received satellite signals by the measurement component based on the received control parameters;
Converting the measurement result of the measurement component into a format suitable for position information calculation in the another processor;
Causing the measurement result of the measurement component to be transferred to the another processor via the interface;
Software code that executes   A computer-readable storage medium in which the software code according to claim 14 is stored. A method in a satellite signal receiver including a measurement component and a first processor comprising:
Receiving control parameters via an interface from another processor external to the satellite signal receiver;
Said first processor controlling measurement of a received satellite signal by said measurement component based on said received control parameter;
Said first processor converting the measurement result of said measurement component into a form suitable for position information calculation in said another processor;
Transferring the measurement result of the measurement component to the another processor via the interface;
Having a method.   17. The method of claim 16, wherein the control parameter includes an indication for a system that performs measurements of received satellite signals among at least two different satellite positioning systems.   The apparatus of claim 1, wherein the measurement result of the measurement component includes decoded navigation information.   The apparatus of claim 1, wherein the apparatus is a satellite signal receiver.   The method of claim 16, wherein the measurement result of the measurement component includes decoded navigation information. Said another processor generating control parameters for said measurement component;
Transmitting control parameters generated by the another processor via the interface to the satellite signal receiver;
Said another processor processing the converted measurement results supplied by said measurement component;
The method of claim 16, further comprising:

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