The present invention relates to a method for tuning a radio filter, especially a radio filter comprising cascade coupled resonator modules. The invention also relates to a radio filter and a system comprising such a radio filter.
The control system in present auto tuned combiners works independently for each resonator module (channel), the phase is measured in each resonator module and the position of the tuning mechanism is adjusted accordingly. In U.S. Pat. No. 6,041,083, by Larsson et al., the processing is done in one control unit, switching between channels, but the measured data and response is for one channel at a time, see FIG. 1.
The problem with the described control system is that it requires a one-to-one correspondence between the position of the tuning mechanism in a certain resonator module and the measured phase. When resonator modules are coupled in cascade, this one-to-one correspondence is no longer possible to find.
A tunable filter is described in U.S. Pat. No. 6,147,577, by W. W. Cavey, which demands an extremely stable environment to operate properly. The described filter has a built-in fault in that the filter doesn't have any possibilities to adjust it self over time, for instance to compensate for temperature drifts.
In U.S. Pat. No. 5,525,940, by Heikkilā et al., and U.S. Pat. No. 5,638,034, by Heikkilā et al., a device and a method for tuning a combiner filter is disclosed. The technique used is tuning on measurement of mainly reflected power from the resonator module.
The present invention seeks to provide a method for tuning a radio filter comprising at least two cascade coupled resonator modules that automatically tunes the filter in response to the input signal to the filter.
According to an aspect of the present invention there is provided a method for tuning a radio filters specified by claim 1.
The invention is also directed to a radio filter.
The invention is further directed to a system comprising a radio filter.
An advantage with the present invention is that the cost for manufacturing radio filters for different operating frequencies, and systems comprising a filter, is reduced since one filter can be used for said different operating frequencies.
Another advantage with the present invention is that the method allows radio filters to be easily tuned, for a specific frequency, in the field, as a response to the input signal(s).
Still another advantage is that the radio filter easily may be tuned to another frequency during operation.
Still another advantage is that the method provides a radio filter to be, during normal operation, adjusted in response to external influence, such as temperature drifts, aging, air humidity, external force.
Each resonator module 12 also includes a separate tuning mechanism 15 (only one tuning mechanism is shown for clarity), and each resonator module is independently tuned by a control unit 16. The signal from each transceiver circuit 13 is sensed and the control unit 16 selects which sensed signal is to be fed into the control unit 16, by setting a signal switch 17 in the desired position. In this example the signal fed into the forth resonator module is sensed by the control unit 16.
A probe (not shown) is provided in each resonator module, which are connected to a probe switch 18. The probes are used to detect the signal within each resonator module, especially when the resonator module 12 is tuned. The signal switch 17 and the probe switch 18 are set in the same position, in this example the fourth position, which means that the signal fed into the fourth resonator module and the signal from the same resonator module are used in the control unit 16 to tune the filter by adjusting the tuning mechanism 15.
The phase value of the signal within each resonator module 12 is used when performing the tuning, since there is a very well defined relationship between the phase of the signal and the position of the tuning mechanism. Each resonator module is tuned to a specific frequency, which corresponds to a specific phase value of the signal within the resonator module. The tuning is performed by measuring the phase value and adjusting the tuning mechanism until the measured phase value corresponds to the desired frequency, i.e. the specific phase value.
A sensor 28 is connected to the control unit 24, which detects if there is any signal Sin coming from the transceiver circuit 21 and furthermore senses the frequency content of signal Sin. The frequency content is used in the control unit to determine the filter frequency, i.e. around which frequency the filter should operate, and as a reference to the measured signals from the probes.
Each probe 26 is used for measuring a signal parameter, e.g. phase or amplitude, at the resonator module, and is connected to the control unit 24 as input signals S1-S4 from each resonator module 25. The control unit provides control signals M1-M4 to the four tuning mechanisms 27.
The input signals Sin, S1, S2, S3, S4 are used to calculate the control signals, which in turn control each tuning mechanism so that the resonator module may be tuned. The tuning is normally performed in two steps, coarse tuning and fine tuning. There are several possible ways of achieving these two steps as illustrated in
The major difference between the described filter in FIG. 2 and the prior art in
When an input signal is fed into the filter, a control unit senses that a signal is present and collects information regarding the frequency content of the signal. This information may be provided as an external signal or determined from the frequency content of the sensed signal.
This information is illustrated as a filter frequency parameter 32, which in this case is a discrete frequency.
The filter characteristic, and thus the filter frequency 30, thereafter automatically moves, as illustrated by the arrows 33, so that the input signal ends up a predetermined distance from the filter frequency 30. Normally the filter frequency 30 overlap the input signal, but in certain cases there is a need to use an offset between them to shift the filter characteristics as described in connection with FIG. 4.
If the input signal is a broad band signal having a carrier signal, the filter frequency parameter 32 may be determined from the average frequency of the input signal or from the carrier frequency.
There is no need for the filter frequency parameter 32 to be within the filter characteristics, as long as the filter frequency parameter 32 may be used to make sure the input signal will be within the filter characteristics when the filter is correctly tuned.
If a portion of a UMTS-band is divided into two equal parts, where a first filter characteristics 41A cover the lower part of the portion up to a cut-off frequency 43 and a second filter characteristics 41B cover the upper part of the portion from the cut-off frequency 43. This means that two filters together covers the portion of the UMTS-band and in this example represents two different operators A and B in the UMTS-band. It is essential for operator A not to transmit or receive signals in the frequency range where the operator A operates, and vice versa.
The UMTS-standard allows each operator A, B to handle up to three different channels, if the bandwidth is e.g. 15 MHz, for transmitting/receiving signals A1-A3, B1-B3. All three channels do not have to be used at the same time by the operator.
The tuning system for operator A senses signals in the allotted frequency range and if operator A only uses channel A3 for sending information, there is a problem with prior art systems in that they normally senses the carrier frequency 44 of channel A3, by determining at which frequency the signal has its maximum amplitude, and lock the filter frequency 42A to the carrier frequency 44. This will cause signals to leak into operator B's allotted frequency range. This is unacceptable for operator B.
The present filter according to the invention has a built-in ability to avoid this to happen. The filter characteristics may be shifted by introducing an offset between the filter frequency 42A and the carrier frequency 44.
The offset to be used, to achieve a filter characteristic as shown in
Both filters for operator A and B are identical in their construction, which means that specially, adapted constructions for different frequencies are not necessary. Only the difference in input signal characteristics will determine the filter characteristics for the respective filter.
In box 53 the control unit determines the frequency content of the detected input signal Sin, which may be done by measuring the frequency content of Sin, and thereby determining a filter frequency, by a frequency counter or by measuring the amplitude of the signal S1 from the first resonator module and calculating a filter frequency, as described in connection with FIG. 6. An alternative way of establishing the filter frequency is to provide an external signal to the control unit, where the purpose of the external signal is to provide the control unit with the desired frequency of the filter independent of the incoming signal Sin.
The flow in
After coarse tuning is done, a signal is present within each resonator modules, which means that a signal parameter, such as amplitude or phase, may be measured at each resonator module. The signal parameter may be measured at the input, the output or inside each resonator module. In the described examples the signal parameter is measured inside the resonator module. The signal parameter is preferably the phase component of the signal.
When the flow continues to box 55, a signal parameter vector {overscore (v)}sp is established by measuring the phase component of the signal within each resonator module. The measured phase components are combined into the vector. Normally a phase reference is needed to establish each phase component and the reference is preferably established by measuring the phase component of the detected signal in box 51. This phase reference value is stored in a memory in the control unit.
The flow continues to box 56 where a set value vector {overscore (v)}sv is established. This step comprises normally of retrieving the set value vector from the memory within the control unit, and the stored set value vector {overscore (v)}sv is determined before hand.
The stored set value vector {overscore (v)}sv is normally frequency dependent, and is preferably expressed as a frequency dependent polynomial or lookup table. However, it is possible to use a frequency independent set value vector within a small frequency range.
The flow continues to box 57 where a relationship between the signal parameter vector {overscore (v)}sp and the set value vector {overscore (v)}sv is defined. The relationship may be defined by using computer simulations, estimations and/or mathematical models. An alternative way of establishing the relationship is to make measurements on a filter when changing the tuning mechanisms in each resonator module as described in connection with FIG. 8.
The relationship between the signal parameter vector {overscore (v)}sp and the set value vector {overscore (v)}sv is preferably arranged into a matrix. The relationship is preferably defined before the tuning of the filter commence, but may take place during the fine tuning procedure. If the relationship is defined before the tuning, the relationship is stored in the memory in the control unit and the step of defining the relationship comprises of retrieving the relationship from the memory.
When the signal parameter vector {overscore (v)}sp, the set value vector {overscore (v)}sv and the relationship are established, a deviation vector between the signal parameter vector {overscore (v)}sp and the set value vector {overscore (v)}sv is calculated using the relationship, see box 58.
If the values in the deviation vector is acceptable, i.e. each signal parameter value is within a predetermined range of the corresponding set value, the flow proceeds via box 59 to box 60, where the flow ends and the filter is correctly tuned. On the other hand if any value of the deviation vector is outside the predetermined range the flow proceeds to box 61, where the tuning mechanisms of the resonator modules are adjusted in response to the deviation values.
After the adjustment is done, the flow continues to box 62 where a new measurement of the signal parameter vector is performed. The flow is fed back to box 58, where a new deviation vector is calculated using the new signal parameter vector. If the values in the deviation vector is within the predetermined range the flow ends in box 60, otherwise the steps 61 and 62 is repeated until all the values in the deviation vector is within the predetermined range.
This process will now be described using the calculated inverse A−1 of the established calibration matrix A as described in connection with
The set value vector {overscore (v)}sv for a filter comprising four cascade coupled resonator modules, where said filter should be tuned for to a filter frequency of 1950 MHz, differs a little from the set value vector at the calibration frequency 1930 MHz which was used in establishing the calibration matrix A. This example will illustrate that the filter will converge to the desired filter frequency through a number of iterations. The set value vector, defining the phase component of the input signal, is:
After coarse tuning the following signal parameter vector {overscore (v)}sp0 was measured:
A deviation vector {overscore (v)}dev0 is then calculated by multiplying the inverse matrix A−1 with the measured signal parameter vector {overscore (v)}sp0.
The deviation matrix is expressed in deviating frequency within each resonator module. The control unit uses the deviation vector to adjust all tuning mechanisms a number of steps corresponding to the deviating frequency.
A new measurement of the signal parameter vector {overscore (v)}sp1 is performed after the first iteration and the calculation process is repeated again. Table 1 shows the result of the iteration process.
The iteration process is terminated after 4 iterations in this example, but more iteration may be performed to obtain an even better result.
If an offset is desirable as discussed in connection with
This is achieved by measuring the amplitude of the signal in the first resonator module, as indicated in box 63, and the adjusting the tuning mechanism of the first resonator module, as indicated in box 64.
The adjustment of the tuning mechanism in box 64 may be terminated when a signal is detected having an amplitude, but the adjustment process is preferably terminated when the amplitude of the measured signal reaches a threshold value or a maximum value.
The filter frequency is thereafter determined, see box 65, by using a relationship between the position of the tuning mechanism in the first resonator module and the filter frequency, e.g. stored in a memory in the control unit. This relationship may be expressed in a table or as a mathematical expression (such as a polynomial).
When the filter frequency is determined, a target position of the other tuning mechanisms are determined, in box 66, by using a similar relationship as the one described above. The relationship between the tuning mechanism and the filter frequency may be different for each resonator module.
When the target position for each tuning mechanism is determined the flow continues to box 67, where the tuning mechanism for each resonator module is adjusted and the flow returns to box 55 in FIG. 5.
When n and k is set, the flow continues to box 71 where the tuning mechanism for resonator module 1 (n=1) is adjusted until an amplitude is detected within the resonator module. The adjustment process is terminated when a signal is detected having an amplitude, but the adjustment process is preferably terminated when the amplitude of the measured signal reaches a threshold value or a maximum value.
The tuning step is repeated for the next resonator module, se box 72 and 73, unless the previously tuned resonator module is the final resonator module, i.e. n=k. In this case the flow is fed back to box 55, FIG. 5.
As previously disclosed in connection with
To be able to perform the fine tuning a set value vector {overscore (v)}sv has to be established, as described in connection with
The relationship may be defined in a number of ways, as described in connection with
The defined relationship is a linear relationship within a small frequency range, and instead of providing a plurality of relationships each adapted for a small frequency range, it is preferred that the defined relationship include comprises frequency dependent variables so that the relationship may be used over a large frequency interval.
The flow starts in box 80, and in box 81 a counter n is set to 1, n=1, and a variable k is set to the present number of resonator modules, in this example k=4. The filter is previously tuned to a calibration frequency, which means that a signal close to the calibration frequency will pass through the filter from the input connection to the output connection. If a specific calibration frequency is not used, the coarse tuning of the filter will provide the same thing as the coarse tuning aim to provide a filter where a signal will pass through.
In the next step, box 82, the signal parameters, in this example the phase component of the signal, in all resonator modules are measured to be used as reference values, or in other words, as a set value vector for this frequency. The following set values illustrates an example for a calibration frequency of 1930 MHz:
The flow then continuos to box 83, where the tuning mechanism for resonator module n=1 is adjusted, or detuned, a predetermined value which corresponds to a frequency response, in this example 0.5 MHz.
The values of the detuned phase component is thereafter measured in all resonator modules, see box 84, and the measured values are arranged in a detuned phase vector {overscore (v)}sp1 in box 85, where sp1 stands for signal parameter in resonator module 1:
After the measurement, the tuning mechanism of resonator module n is optionally adjusted back to the value before the detuning operation started.
In box 86 the method determines if the previous measurement was made for the final resonator module. If not, the flow is fed back via box 87, where the counter n is increased by 1, and box 83-86 is repeated for n=2.
The tuning mechanism of resonator module 2 is detuned a predetermined value, which may differ from the detuned value of the first resonator module, corresponding to the same frequency response as for the first resonator module. The phase component is measured in all resonator modules, arranged in a vector and the tuning mechanism is adjusted back.
The additional detuned phase vectors was measured when k=4:
When n=k in box 86, the flow continues to box 88, where the measured detuned phase vectors are normalized by subtracting the set value vector from each detuned phase vector and thereafter dividing it by the frequency response for each detuning.
The final step for achieving a calibration matrix is to arrange the normalized detuned phase vectors in a matrix, as performed in box 89. The resulting calibration matrix has the following values:
To be able to use the established calibration matrix, an inverse has to be calculated, which is performed in box 90, having the following values:
The flow ends in box 91.
The above described process for obtaining a relationship between the set value vector and the measured signal parameter vector is performed by adjusting a tuning mechanism at a time. An alternative way of establishing the relationship is to adjust two tuning mechanisms at a time, as long as the adjustments have a linear independent relationship. This could be obtained by making the adjustments for a filter comprising four resonator modules:
A control unit 24 is provided, which receive information from the resonator modules from the probes 26 and a sensor 28 at the input connection 95 measures a reference signal Sref, as previously described in connection with FIG. 2.
The control unit 24 is also connected to the isolation circuit 94. A detection signal Sdet, which is essentially a small fraction of the input signal(s) Sin is forwarded to the control unit. The detection signal is used to detect if a signal is present and to determine the frequency content of the input signal(s).
A relationship between a set value vector and a signal parameter vector may be established in the same way as described in connection with
The relationship between the set value vector and the signal parameter vector in
The control unit 24 is furthermore connected to the sensor 28, to establish a reference value as described in connection with
The first, second and final resonator module 1311-1313 are provided with a tuning mechanism (not shown), but only the first and the second resonator is provided with a probe 26. The non-tunable resonator module 132 is connected to the final resonator module 1313 as a notch resonator. The output connection 97 is connected to a second non-tunable resonator module 133, which is provided with a probe 26, cascade coupled to a third non-tunable resonator module 134. The output from the third non-tunable resonator module is connected to an antenna system (not shown).
The control unit 24 receive signals from the sensor 28, as described in connection with
The control unit senses the frequency content of the signal from the transmitter 141 and tunes automatically the filter 144, as previously described.
The system 140 further comprises a second filter 147 being connected between said antenna 146 and a receiver 148, and a slave unit 149 being connected to said control unit 145 and said second filter 147. The control unit 145 provides the slave unit 149 with information regarding tuning values for the resonator modules within the second filter 147. This may be determined in some systems where there is a predetermined frequency shift between the transmitting link and the receiving link.
The coupling structure is a combiner structure, as described in
Each filter may be tuned to a separate frequency, and thereby create a system function as illustrated in FIG. 16. The x-axis is frequency f and the y-axis is transmission in dB. The system function comprises two separate filter functions 161 and 162.
Another frequency diagram is shown in
Although most examples indicate that the signal parameter inside the resonator module is directly measured, this is normally not the case. A cable or even a fixed resonator module, as shown in
Further, the described embodiments of the present invention illustrate a probe being attached to each resonator, but the scope of the invention should not be limited to this. Any type of probe or sensor that may be used to measure signal parameters at each resonator, e.g. sensors provided at the output of the resonators, probes provided within the resonators, may be used.
In the embodiments described above where all tunable resonator modules are provided with a probe, it is possible to tune the filter to a specific filter frequency, even though the measured signal parameter from a resonator module is faulty. This may be the case when a probe is damaged and the measured signal parameter is not representative to the actual signal parameter present within the resonator module.
Simulations have shown that when this occurs, the filter will still converge after an increased number of iterations, such as ten times as many as usual, due to that the used matrix include additional information regarding all present tunable resonator modules and their internal relationship.
The radio filter is preferably operational in a frequency range between 100 MHz and 3 GHz, but may operate at a frequency of 3 GHz or higher. A radio filter may be any type of filter working in the microwave range, including radio filters designed for telecommunication purposes, such as telephony and data communications.
Number | Date | Country | Kind |
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0004658 | Dec 2000 | SE | national |
This is a nationalization of PCT/SE01/02758 filed Dec. 12, 2001 and published in English.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/SE01/02758 | 12/12/2001 | WO | 00 | 10/31/2003 |
Publishing Document | Publishing Date | Country | Kind |
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WO02/49213 | 6/20/2002 | WO | A |
Number | Name | Date | Kind |
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3715690 | Young et al. | Feb 1973 | A |
4692724 | Harris | Sep 1987 | A |
5065121 | Ghadaksaz | Nov 1991 | A |
5525940 | Heikkila et al. | Jun 1996 | A |
5638034 | Heikkila et al. | Jun 1997 | A |
6041083 | Larsson et al. | Mar 2000 | A |
6147577 | Cavey | Nov 2000 | A |
Number | Date | Country |
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1253306 | Nov 1971 | GB |
WO0064052 | Oct 2000 | WO |
Number | Date | Country | |
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20040061567 A1 | Apr 2004 | US |