Subversion Repositories svnkaklik

Rev

Rev 1104 | Rev 1107 | Go to most recent revision | Show entire file | Ignore whitespace | Details | Blame | Last modification | View Log

Rev 1104 Rev 1105
Line 1... Line 1...
1
\chap Trial design
1
\chap Trial design
2
 
2
 
3
The whole design of radioastronomy receiver digitalization unit is constructed to be used in a wide range of applications and tasks related to digitalisation of signal from radioastronomy receivers. A good illustrating problem for its use is a signal digitalisation from multiple antenna arrays. This design will eventually become a part of MLAB Advanced Radio Astronomy System. 
3
The whole design of radioastronomy receiver digitalization unit is constructed to be used in a wide range of applications and tasks related to digitalization of signal from radioastronomy receivers. A good illustrating problem for its use is a signal digitalisation from multiple antenna arrays. This design will eventually become a part of MLAB Advanced Radio Astronomy System. 
4
 
4
 
5
\sec Required parameters
5
\sec Required parameters
6
 
6
 
7
Wide dynamical range and high IP3 are desired. The receiver must accept wide dynamic signals because a typical radioastronomical signal has a form of a weak signal covered by a strong man-made noise.    
7
Wide dynamical range and high IP3 are desired. The receiver must accept wide dynamic signals because a typical radioastronomical signal has a form of a weak signal covered by a strong man-made noise.    
8
 
8
 
Line 29... Line 29...
29
 
29
 
30
Clock signal will be handled distinctively in our scalable design. Selected ADC chip are guaranteed to have defined clock skew between sampling and data output clock. This allows taking data and frame clocks from the first ADC module only. The rest of the data and frame clocks from other ADC modules can be measured for diagnostic purposes (failure detection, jitter measurement etc.).
30
Clock signal will be handled distinctively in our scalable design. Selected ADC chip are guaranteed to have defined clock skew between sampling and data output clock. This allows taking data and frame clocks from the first ADC module only. The rest of the data and frame clocks from other ADC modules can be measured for diagnostic purposes (failure detection, jitter measurement etc.).
31
 
31
 
32
This system concept allows for scalability, that is technically limited by a number of differential signals on host side and its computational power.  There is another advantage of scalable data acquisition system -- an economic one. Observatories or end users can make a choice of how much money are they willing to spent on radioastronomy receiver system. This freedom of choice is especially useful for science sites without previous experience in radioastronomy observations.     
32
This system concept allows for scalability, that is technically limited by a number of differential signals on host side and its computational power.  There is another advantage of scalable data acquisition system -- an economic one. Observatories or end users can make a choice of how much money are they willing to spent on radioastronomy receiver system. This freedom of choice is especially useful for science sites without previous experience in radioastronomy observations.     
33
 
33
 
34
\secc Differential signalling 
34
\secc Differential signaling 
35
 
35
 
36
The concept of scalable design requires relatively long circuit traces between ADC and digital unit which captures the data and performs the computations. The long distance between the digital processing unit and the analog-to-digital conversion unit has an advantage in noise retention typically produced by digital circuits. Those digital circuits, such as FPGA or other flip-flops block and circuit traces, usually work at high frequencies and emit wide-band noise with relatively low power. In such cases any increase in a distance between the noise source and analog signal source increase S/N significantly. However, at the same time a long distance brings problems with the digital signal transmission between ADC and computational unit. This obstacle should be resolved more easily in free-space than on board routing. The high-quality differential signalling shielded cables should be used. This technology has two advantages over PCB signal routing. First, it can use twisted pair of wires for leak inductance suppression in signal path and second, the twisted pair may additionally be shielded by uninterrupted metal foil.              
36
The concept of scalable design requires relatively long circuit traces between ADC and digital unit which captures the data and performs the computations. The long distance between the digital processing unit and the analog-to-digital conversion unit has an advantage in noise retention typically produced by digital circuits. Those digital circuits, such as FPGA or other flip-flops block and circuit traces, usually work at high frequencies and emit wide-band noise with relatively low power. In such cases any increase in a distance between the noise source and analog signal source increase S/N significantly. However, at the same time a long distance brings problems with the digital signal transmission between ADC and computational unit. This obstacle should be resolved more easily in free-space than on board routing. The high-quality differential signalling shielded cables should be used. This technology has two advantages over PCB signal routing. First, it can use twisted pair of wires for leak inductance suppression in signal path and second, the twisted pair may additionally be shielded by uninterrupted metal foil.              
37
 
37
 
38
\secc Phase matching
38
\secc Phase matching
39
 
39
 
40
For multiple antenna radioastronomy projects, system phase stability is a mandatory condition. It allows precise high resolution imaging of objects. 
40
For multiple antenna radioastronomy projects, system phase stability is a mandatory condition. It allows precise high resolution imaging of objects. 
41
 
41
 
42
High phase stability in our scalable design is achieved through centralised frequency generation  and distribution with multi-output LVPECL hubs, that have equiphased outputs for multiple devices. 
42
High phase stability in our scalable design is achieved through centralized frequency generation  and distribution with multi-output LVPECL hubs, that have equiphased outputs for multiple devices. 
43
 
43
 
44
This design ensures that all devices have access to the defined phase and known frequency.     
44
This design ensures that all devices have access to the defined phase and known frequency.     
45
 
45
 
46
 
46
 
47
\sec System description
47
\sec System description
48
 
48
 
49
In this section testing system will be described.
49
In this section testing system will be described.
50
 
50
 
51
\secc Frequency synthesis       
51
\secc Frequency synthesis       
52
 
52
 
53
We have used a centralised topology as a basis for frequency synthesis. One precise high-frequency and low-jitter digital oscillator has been used, while other working frequencies have been derived from it by the division of its signal. This central oscillator has a software defined GPS disciplined control loop for frequency stabilisation.\fnote{\url{http://wiki.mlab.cz/doku.php?id=en:gpsdo} SDGPSDO design has been developed in parallel to this diploma thesis as a related project, but it is not explicitly required by the diploma thesis.}
53
We have used a centralized topology as a basis for frequency synthesis. One precise high-frequency and low-jitter digital oscillator has been used, while other working frequencies have been derived from it by the division of its signal. This central oscillator has a software defined GPS disciplined control loop for frequency stabilization.\fnote{\url{http://wiki.mlab.cz/doku.php?id=en:gpsdo} SDGPSDO design has been developed in parallel to this diploma thesis as a related project, but it is not explicitly required by the diploma thesis.}
54
We have used methods of frequency monitoring compensation in order to meet modern requirements on radioastronomy equipment which needs precise frequency and phase stability over a wide scale for effective radioastronomy imaging. 
54
We have used methods of frequency monitoring compensation in order to meet modern requirements on radioastronomy equipment which needs precise frequency and phase stability over a wide scale for effective radioastronomy imaging. 
55
 
55
 
56
Every ADC module will be directly connected to CLKHUB02A module which takes sampling clock signal delivered by FPGA from main local oscillator.  This signal should use high quality differential signalling cable -- we should use SATA cable for this purpose. 
56
Every ADC module will be directly connected to CLKHUB02A module which takes sampling clock signal delivered by FPGA from main local oscillator.  This signal should use high quality differential signaling cable -- we should use SATA cable for this purpose. 
57
 
57
 
58
GPSDO design included in data acquisition system has special feature -- generates time marks for precise time-stamping of received signal. Timestamps are created by disabling of local oscillator for 100 us as result rectangle click in input signal is created which appears as horizontal line in spectrogram.   
58
GPSDO design included in data acquisition system has special feature -- generates time marks for precise time-stamping of received signal. Timestamps are created by disabling of local oscillator for 100 us as result rectangle click in input signal is created which appears as horizontal line in spectrogram.   
59
Timestamps should be seen in image \ref[meteor-reflection] (above and below meteor reflection).
59
Timestamps should be seen in image \ref[meteor-reflection] (above and below meteor reflection).
60
 
60
 
61
Time-marking should be improved in future by digitalisation GPS signal directly with dedicated ADC channel.  Datafile then consists samples from channels of radio-astronomy receivers along with GPS signal containing precise time information. 
61
Time-marking should be improved in future by digitalisation GPS signal directly with dedicated ADC channel.  Datafile then consists samples from channels of radio-astronomy receivers along with GPS signal containing precise time information. 
Line 80... Line 80...
80
\picw=10cm \cinspic ./img/miniSAS_SATA_cable.jpg
80
\picw=10cm \cinspic ./img/miniSAS_SATA_cable.jpg
81
\caption/f A type of miniSAS cable similar to used.
81
\caption/f A type of miniSAS cable similar to used.
82
\endinsert
82
\endinsert
83
 
83
 
84
\secc Signal integrity requirements
84
\secc Signal integrity requirements
-
 
85
\label[diff-signaling]
85
 
86
 
86
We use ADC modules that have DATA clock frequency eight times higher than sampling frequency in single line output mode, implying a 40 MHz output bit rate. 
87
We use ADC modules that have DATA clock frequency eight times higher than sampling frequency in single line output mode, implying a 40 MHz output bit rate. This imply $ 1/4*10^7 = 25$ ns time length of data bit, which is equivalent to 7.5m light path in free space. If we use copper PCB with FR4 substrate layer or coaxial/twinax cable, we could obtain velocity factor of 0.66 at worst condition. Then the light path for the same bit rate will be 4.95 m. Although we do not have any cables in system with comparable lengths, worst data bit skew described by data sheets of used components is $0.3*sample time$ time which is 1.485 m. Therefore length matching is not critical in our design. 
87
 
88
 
88
 
89
 
89
\secc ADC modules design
90
\secc ADC modules design
90
 
91
 
91
The ADC modules have a standard MLAB construction scheme with four mounting holes in corners aligned in defined raster. 
-
 
92
 
-
 
93
Data serial data outputs of ADC modules should be connected directly to FPGAs for the basic primary signal processing. The ADC chip used in the modules has a selectable bit width of data output bus and thus the output SATA connectors have signals arranged to contain a single bit from every ADC channel.  This creates a signal concept enabling a selection of a proper bus bit-width according to the sampling rate (higher bus bit-width downgrades signalling speed and vice versa.)
-
 
94
 
-
 
95
In order to connect the above mentioned signalling layout, miniSAS to multiple SATA cable should be used.  
-
 
96
 
-
 
97
A KiCAD design suite had been chosen for PCB layout. However, the version is, despite having integrated CERN Push \& Shove routing capability, slightly unstable as it sometimes crushes due to an exception during routing. On the basis of these stability issues, the design had to be saved quite often. On the other hand, compared to commercially available solutions, such as MentorGraphics PADS or Cadence Orcad,  the Open-source KiCAD provides an acceptable option and it easily surpasses a widely used Eagle software.
-
 
98
 
-
 
99
As a part of work on the thesis, new PCB footprints for FMC, SATA a and miniSAS connectors have been designed and were committed to KiCAD github library repository. They are now publicly available on the official KiCAD repository at GitHub.  
-
 
100
 
-
 
101
 
92
 
102
\secc ADC selection
93
\secc ADC selection
103
 
94
 
104
There exist several ADC signalling formats currently used in communication with FPGA. 
95
There exist several ADC signaling formats currently used in communication with FPGA. 
105
 
96
 
106
\begitems
97
\begitems
107
  * DDR LVDS
98
  * DDR LVDS
108
  * JEDEC 204B
99
  * JEDEC 204B
109
  * JESD204A
100
  * JESD204A
Line 114... Line 105...
114
 
105
 
115
Because it uses the smallest number of differential pairs, the choice fell on the serial LVDS format. Small number of differential pairs is an important parameter determining the construction complexity and reliability. \url{http://www.ti.com/lit/pdf/snaa110}
106
Because it uses the smallest number of differential pairs, the choice fell on the serial LVDS format. Small number of differential pairs is an important parameter determining the construction complexity and reliability. \url{http://www.ti.com/lit/pdf/snaa110}
116
 
107
 
117
An ultrasound AFE chip seems to be ideal for this purpose -- the chip has integrated both front-end amplifiers and filters. It has a drawback though - it is incapable of handling differential input signal and has a relatively low dynamic range (as it consists only of 12bit ADC). Because this IO has many ADC channels the scaling is possible only by a factor of 4 receivers (making 8 analogue channels).
108
An ultrasound AFE chip seems to be ideal for this purpose -- the chip has integrated both front-end amplifiers and filters. It has a drawback though - it is incapable of handling differential input signal and has a relatively low dynamic range (as it consists only of 12bit ADC). Because this IO has many ADC channels the scaling is possible only by a factor of 4 receivers (making 8 analogue channels).
118
 
109
 
119
If we require a separate output for every analogue channel and a 16bit depth we find that there are only a few 2-Channel simultaneous sampling ADCs currently existing which meet these requirements.  We have summarised the ADCs in the following table \ref[ADC-type] 
110
If we require a separate output for every analogue channel and a 16bit depth we find that there are only a few 2-Channel simultaneous sampling ADCs currently existing which meet these requirements.  We have summarized the ADCs in the following table \ref[ADC-type] 
120
 
111
 
121
\midinsert \clabel[ADC-types]{Available ADC types}
112
\midinsert \clabel[ADC-types]{Available ADC types}
122
\ctable{lrrrrrcc}{
113
\ctable{lrrrrrcc}{
123
\hfil ADC Type & LTC2271 & LTC2190 & LTC2191 & LTC2192 & LTC2193 & LTC2194 & LTC2195 \cr
114
\hfil ADC Type & LTC2271 & LTC2190 & LTC2191 & LTC2192 & LTC2193 & LTC2194 & LTC2195 \cr
124
SNR [dB] & 84.1 & 77 & 77 & 77 & 76.8 & 76.8 & 76.8 \cr
115
SNR [dB] & 84.1 & 77 & 77 & 77 & 76.8 & 76.8 & 76.8 \cr
Line 131... Line 122...
131
\caption/t The summary of available ADC types and theirs characteristics. 
122
\caption/t The summary of available ADC types and theirs characteristics. 
132
\endinsert
123
\endinsert
133
 
124
 
134
All parts in this category are compatible with one board layout. Main differences lay in the sampling frequency and signal to noise ratio, with the slowest having a maximum sampling frequency of 20 MHz. However all of them have a minimal sampling frequency of 5 MSPS and all are configurable over a serial interface (SPI). SPI seems to be a standard interface used in high-end ADC chips made by the largest manufacturers (Analog Devices, Linear technology, Texas instruments, Maxim integrated..). 
125
All parts in this category are compatible with one board layout. Main differences lay in the sampling frequency and signal to noise ratio, with the slowest having a maximum sampling frequency of 20 MHz. However all of them have a minimal sampling frequency of 5 MSPS and all are configurable over a serial interface (SPI). SPI seems to be a standard interface used in high-end ADC chips made by the largest manufacturers (Analog Devices, Linear technology, Texas instruments, Maxim integrated..). 
135
 
126
 
-
 
127
 
-
 
128
 
-
 
129
The ADC modules have a standard MLAB construction scheme with four mounting holes in corners aligned in defined raster. 
-
 
130
 
-
 
131
Data serial data outputs of ADC modules should be connected directly to FPGAs for the basic primary signal processing. The ADC chip used in the modules has a selectable bit width of data output bus and thus the output SATA connectors have signals arranged to contain a single bit from every ADC channel.  This creates a signal concept enabling a selection of a proper bus bit-width according to the sampling rate (higher bus bit-width downgrades signalling speed and vice versa.)
-
 
132
 
-
 
133
In order to connect the above mentioned signalling layout, miniSAS to multiple SATA cable should be used.  
-
 
134
 
-
 
135
A KiCAD design suite had been chosen for PCB layout. However, the version is, despite having integrated CERN Push \& Shove routing capability, slightly unstable as it sometimes crushes due to an exception during routing. On the basis of these stability issues, the design had to be saved quite often. On the other hand, compared to commercially available solutions, such as MentorGraphics PADS or Cadence Orcad,  the Open-source KiCAD provides an acceptable option and it easily surpasses a widely used Eagle software.
-
 
136
 
-
 
137
As a part of work on the thesis, new PCB footprints for FMC, SATA a and miniSAS connectors have been designed and were committed to KiCAD github library repository. They are now publicly available on the official KiCAD repository at GitHub.  
-
 
138
 
-
 
139
 
-
 
140
 
-
 
141
ADCdual01A module has several digital data output formats
-
 
142
 
-
 
143
\begitems
-
 
144
    * 1-lane mode
-
 
145
\enditems
-
 
146
 
-
 
147
All of these modes are supported by module design. For discused data acquisition system the 1-lane mode was selected. 1-lane mode allows minimal number of differential pairs between ADCdual01A and FPGA. Digital signaling scheme used in 1-lane mode is shown in image \ref[1-line-out]. 
-
 
148
 
-
 
149
\midinsert
-
 
150
\clabel[1-line-out]{Single line ADC output signals}
-
 
151
\picw=15cm \cinspic ./img/ADC_single_line_output.png
-
 
152
\caption/f Digital signaling shema for  1-line  ADC digital output mode.
-
 
153
\endinsert
-
 
154
 
-
 
155
ADCdual01A parameters can be set either by jumper setup (refered as parallel programming  in device's data sheet) or by SPI interface. SPI interface has been selected for our system, because parallel programming lacks of options (test pattern output setup for example). 
-
 
156
 
-
 
157
Complete schematic diagram of ADCdual01A module board is included in the appendix. 
-
 
158
 
-
 
159
 
136
\secc ADC modules interface
160
\secc ADC modules interface
137
 
161
 
138
Both of the ADCdual01A modules were connected to FPGA ML605 board trough FMC2DIFF01A adapter board. The design of this adapter module expects the presence of FMC LPC connector and the board is, at the same time, not compatible with MLAB. It is, on the other hand, designed to meet the VITA 57 standard specifications for boards which support region 1 and region 3. VITA 57 regions are explained in the picture \ref[VITA57-regions].
162
Both of the ADCdual01A modules were connected to FPGA ML605 board trough FMC2DIFF01A adapter board. The design of this adapter module expects the presence of FMC LPC connector and the board is, at the same time, not compatible with MLAB. It is, on the other hand, designed to meet the VITA 57 standard specifications for boards which support region 1 and region 3. VITA 57 regions are explained in the picture \ref[VITA57-regions].
139
This industry standard guarantees the compatibility with other FPGA boards that have FMC LPC connectors for Mezzanine Card. Schematic diagram of this adapter board is included in the appendix. 
163
This industry standard guarantees the compatibility with other FPGA boards that have FMC LPC connectors for Mezzanine Card. Schematic diagram of designed adapter board is included in the appendix. 
140
 
164
 
141
The primary purpose of the PCB is to enable the connection of ADC modules located outside the PC case. (In PC box analog circuits cannot be realised without the use of massive RFI mitigation techniques). 
165
The primary purpose of the PCB is to enable the connection of ADC modules located outside the PC case. (In PC box analog circuits cannot be realised without the use of massive RFI mitigation techniques). 
142
Differential signalling connectors should be used for conducting digital signal over relatively long cables. The signal integrity sensitive links (clocks) are equipped with output driver and translator to LVPECL logic for better signal transmission quality.  
166
Differential signalling connectors should be used for conducting digital signal over relatively long cables. The signal integrity sensitive links (clocks) are equipped with output driver and translator to LVPECL logic for better signal transmission quality.  
143
 
167
 
144
\midinsert
168
\midinsert
Line 152... Line 176...
152
\caption/f Definition of VITA57 regions.
176
\caption/f Definition of VITA57 regions.
153
\endinsert
177
\endinsert
154
 
178
 
155
Several SATA connectors and two miniSAS connectors are populated on this board.  This set of connectors allows a connection of any number of ADC modules within the range of 1 to 8. ADC data outputs should be connected to the miniSAS connectors, while other supporting signals should be routed directly to SATA connectors on adapter. 
179
Several SATA connectors and two miniSAS connectors are populated on this board.  This set of connectors allows a connection of any number of ADC modules within the range of 1 to 8. ADC data outputs should be connected to the miniSAS connectors, while other supporting signals should be routed directly to SATA connectors on adapter. 
156
 
180
 
157
Differential pairs routed on PCB are not matched for lenghts. Althought inter differential pairs 
181
Lengths of differential pairs routed on PCB of module are not matched between pairs. Length variation of differential pairs is not critical in our design according to facts discussed in paragraph \ref[diff-signaling]. Nevertheless signals within differential pairs itself are matched for length. Internal signal traces length mating of differential pairs is mandatory in order to avoid dynamic logic hazard conditions on digital signals. Thus clocks signals are routed most precisely on all designed boards.
158
 
-
 
159
 
182
 
160
 
183
 
161
Signal configuration used in our trial design is described in the following tables. 
184
Signal configuration used in our trial design is described in the following tables. 
162
 
185
 
163
\secc Output data format
186
\secc Output data format
Line 191... Line 214...
191
 
214
 
192
Interactive grabber viewer user interface shows live oscilloscope-like time-value display for all data channels and live time-frequency scrolling display (a waterfall view) for displaying the frequency components of the grabbed signal. 
215
Interactive grabber viewer user interface shows live oscilloscope-like time-value display for all data channels and live time-frequency scrolling display (a waterfall view) for displaying the frequency components of the grabbed signal. 
193
 
216
 
194
\secc ADC module parameters
217
\secc ADC module parameters
195
 
218
 
196
Two pieces of ADC modules were completed and tested. The first piece, labeled ADC1, has LTC21190
219
Two pieces of ADC modules were completed and tested. The first piece, labeled ADC1, has LTC2190
197
ADC chip populated with LT6600-5 front-end operational amplifier. It also has a 1kOhm resistors populated on inputs which gives it an ability of an internal attenuation of input signal. The value of this attenuation $A$ is described by the following formula 
220
ADC chip populated with LT6600-5 front-end operational amplifier. It also has a 1kOhm resistors populated on inputs which gives it an ability of an internal attenuation of input signal. The value of this attenuation $A$ is described by the following formula \ref[ADC1-gain]
198
 
-
 
199
 
-
 
200
\midinsert
-
 
201
\picw=15cm \cinspic ./img/screenshots/ADC1_CH2_FFT.png
-
 
202
\caption/f Sine signal sampled by ADC1 module with LTC21190 and LT6600-5 devices.
-
 
203
\endinsert
-
 
204
 
-
 
205
 
-
 
206
ADC1 CH1  maximal input 705.7 mV
-
 
207
 
-
 
208
 
-
 
209
 
221
 
-
 
222
\label[ADC1-gain]
210
$$
223
$$
211
A = {1580 \times R_1 \over R_1 + R_2}
224
A = {806 \times R_1 \over R_1 + R_2}
212
$$
225
$$
213
 
226
 
214
Where is 
227
Where is 
215
\begitems
228
\begitems
216
  * $A$ -  Gain of input aplifier.
229
  * $A$ -  Gain of input amplifier.
217
  * $R_1$ - Output impedance of signal source (usually 50 Ohm).
230
  * $R_1$ - Output impedance of signal source (usually 50 Ohm).
218
  * $R_2$ - Value of serial resitors at operational apmlifier inputs.
231
  * $R_2$ - Value of serial resistors at operational amplifier inputs.
219
\enditems
232
\enditems
220
 
233
 
-
 
234
We have $R_2 = 1000 \Omega$ and $R_1 = 50 \Omega$ which imply $A = 0.815$. That value of A is confirmed by measurement. 
-
 
235
In our measurement setup we have H1012 Ethernet transformer connected at inputs of ADC. Transformer has 10\% tolerance in impedance and amplification. We measured ADC saturation voltage 705.7 mV (generator output) in this setup due to impedance mismatch and uncalibrated transformer gain. 
-
 
236
 
221
 
237
 
222
\midinsert
238
\midinsert
-
 
239
\clabel[ADC1-FFT]{ADC1 sine test FFT}
223
\picw=15cm \cinspic ./img/screenshots/ADC2_CH1_FFT.png
240
\picw=15cm \cinspic ./img/screenshots/ADC1_CH2_FFT.png
224
\caption/f Sine signal sampled by ADC2 module with LTC2271 and LT6600-2.5 devices.
241
\caption/f Sine signal sampled by ADC1 module with LTC2190 and LT6600-5 devices.
225
\endinsert
242
\endinsert
226
 
243
 
227
1k
-
 
228
 
-
 
229
ADC2 CH1 maximal input 380 mV
-
 
230
 
244
 
-
 
245
For ADC2 we must use formula with different constant \ref[ADC1-gain]. ADC2 module has LT6600-2.5 populated and gain is $A = 2.457$ with same $R_2$ resistors. We measured saturation voltage of 380 mV (generator output) at channel 1 on this ADC. It is well in parameter tolerances  of used setup.   
231
 
246
 
-
 
247
\label[ADC2-gain]
232
$$
248
$$
233
A = {806 \times R_1 \over R_1 + R_2}
249
A = {1580 \times R_1 \over R_1 + R_2}
234
$$
250
$$
235
 
251
 
236
Where is 
252
Where is 
237
\begitems
253
\begitems
238
  * $A$ -  Gain of input aplifier.
254
  * $A$ -  Gain of input amplifier.
239
  * $R_1$ - Output impedance of signal source (usually 50 Ohm).
255
  * $R_1$ - Output impedance of signal source (usually 50 Ohm).
240
  * $R_2$ - Value of serial resitors at operational apmlifier inputs.
256
  * $R_2$ - Value of serial resistors at operational amplifier inputs.
241
\enditems
-
 
242
 
-
 
243
Both images confirms that ADC modules have input dynamical range 80 dB at least. 
-
 
244
 
-
 
245
 
-
 
246
 
-
 
247
ADCdual01A module has several digital data output formats
-
 
248
\begitems
-
 
249
    * 1-lane mode
-
 
250
\enditems
257
\enditems
251
 
258
 
-
 
259
\midinsert
-
 
260
\clabel[ADC2-FFT]{ADC2 sine test FFT}
-
 
261
\picw=15cm \cinspic ./img/screenshots/ADC2_CH1_FFT.png
252
All of these modes are supported by module design. For discused data aquisition system the 1-lane mode was selected. 1-lane mode allows minimal number of diff pais between ADCdual01A and FPGA. 
262
\caption/f Sine signal sampled by ADC2 module with LTC2271 and LT6600-2.5 devices.
-
 
263
\endinsert
253
 
264
 
254
ADCdual01A parameters can be set either by jupmper setup (refered as parallel pragramming  in device's datasheet) or by SPI interface. SPI interface has been selected for our system, because papralel programming lacks of option of test pattern output setup. 
265
Computed FFT spectra for measured signal are shown in images \ref[ADC2-FFT] and \ref[ADC1-FFT].  Both images confirms that ADCdual01A modules have input dynamical range 80 dB at least. 
255
 
266
 
256
\chap Example of usage
267
\chap Example of usage
257
 
268
 
258
%\sec Simple polarimeter station
269
For additional validation of system design a receiver setup was constructed. 
259
    
270
    
260
\sec Basic interferometer station
271
\sec Basic interferometer station
261
 
272
 
262
For system evaluation basic interferometry station was constructed.
273
Interferometry station was selected as most basic setup. We connected the new data acquisition system to two SDRX01B receivers. Block schematic of used setup is shown in image \ref[block-schematic]. Two ground-plane antennas were used and mounted outside of balcony at CTU building at location 50°4'36.102"N, 14°25'4.170"E. Antennas were equipped  by LNA01A amplifiers. Coaxial cable length are matched for 5 meters. And antennas were isolated by common mode ferrite bead mounted on cable for minimize signal coupling between antennas. Evaluation system consists SDGPSDO local oscillator subsystem used for tunning local oscillator frequency. 
-
 
274
 
-
 
275
\midinsert
-
 
276
\clabel[block-schematic]{Receiver block schematic}
-
 
277
\picw=10cm \cinspic ./img/Coherent_UHF_SDR_receiver.png
-
 
278
\caption/f Complete receiver block schematic of dual antenna interferometric station.
-
 
279
\endinsert
-
 
280
 
-
 
281
 
263
 
282
 
264
\midinsert
283
\midinsert
265
\clabel[meteor-reflection]{Meteor reflection}
284
\clabel[meteor-reflection]{Meteor reflection}
266
\picw=10cm \cinspic ./img/screenshots/observed_meteor.png
285
\picw=10cm \cinspic ./img/screenshots/observed_meteor.png
267
\caption/f Meteor reflection received by evaluation setup.
286
\caption/f Meteor reflection received by evaluation setup.
Line 272... Line 291...
272
\picw=10cm \cinspic ./img/screenshots/phase_difference.png
291
\picw=10cm \cinspic ./img/screenshots/phase_difference.png
273
\caption/f Demonstration of phase difference between antennas.
292
\caption/f Demonstration of phase difference between antennas.
274
\endinsert
293
\endinsert
275
 
294
 
276
 
295
 
277
\midinsert
-
 
278
\clabel[block-schematic]{Receiver block schematic}
-
 
279
\picw=10cm \cinspic ./img/Coherent_UHF_SDR_receiver.png
-
 
280
\caption/f Complete receiver block schematic of dual antenna interferometric station.
-
 
281
\endinsert
-
 
282
 
-
 
283
 
296
 
284
%\sec Simple passive Doppler radar
297
%\sec Simple passive Doppler radar
285
 
298
 
-
 
299
%\sec Simple polarimeter station
-
 
300
 
286
\chap Proposed final system
301
\chap Proposed final system
287
 
302
 
288
Construction of a final system which is supposed to be employed for real radioastronomy observations will be described. This chapter is mainly a theoretical analysis of data handling systems. Realisation of these ideas might be possible as a part of our future development after we fully evaluate and test the current trial design. 
303
Construction of a final system which is supposed to be employed for real radioastronomy observations will be described. This chapter is mainly a theoretical analysis of data handling systems. Realization of these ideas might be possible as a part of our future development after we fully evaluate and test the current trial design. 
289
 
304
 
290
\sec Custom design of FPGA board
305
\sec Custom design of FPGA board
291
 
306
 
292
In the beginning of the project, a custom design of FPGA interface board had been considered. This FPGA board should include PCI express interface and should sell at lower price than trial design. It should be compatible with MLAB which is further backward compatible with the existing or improved design of ADC modules. For a connection of this board to another adapter board with PCIe we expect a use of a host interface. 
307
In the beginning of the project, a custom design of FPGA interface board had been considered. This FPGA board should include PCI express interface and should sell at lower price than trial design. It should be compatible with MLAB which is further backward compatible with the existing or improved design of ADC modules. For a connection of this board to another adapter board with PCIe we expect a use of a host interface. 
293
Thunderbolt technology standard was expected to be used in this PC to PCIe -> FPGA module. Thunderbolt chips are currently available on the market for reasonable prices. However, a problem lies in the accessibility to their specifications, as they are only available for licensed users and Intel has a mass market oriented licensing policy, that makes this technology inaccessible for low quantity production. As a consequence, an external PCI Express cabling and expansion slots should be considered as a better solution. 
308
Thunderbolt technology standard was expected to be used in this PC to PCIe -> FPGA module. Thunderbolt chips are currently available on the market for reasonable prices. However, a problem lies in the accessibility to their specifications, as they are only available for licensed users and Intel has a mass market oriented licensing policy, that makes this technology inaccessible for low quantity production. As a consequence, an external PCI Express cabling and expansion slots should be considered as a better solution.