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            | 1 | \chap Trial version of the digitizer
 | 1 | \chap Trial version of the digitizer
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            | 3 | The whole design of the radioastronomic receiver digitization unit is meant to be used in a wide range of applications and tasks related to digitization of a signal. A good illustrating problem for its use is the signal digitization from multiple antenna arrays. Design and implementation of the system is presented in this chapter.
 | 3 | The whole design of the radioastronomic receiver digitization unit is meant to be used in a wide range of applications and tasks related to digitization of a signal. A good illustrating problem for its use is the signal digitization from multiple antenna arrays. Design and implementation of the system is presented in this chapter.
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            | 5 | \midinsert
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            | 6 | \clabel[expected-block-schematic]{Expected system block schematic}
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            | 7 | \picw=\pdfpagewidth \setbox0=\hbox{\inspic ./img/Coherent_UHF_SDR_receiver.png }
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            | 8 | \par\nobreak \vskip\wd0 \vskip-\ht0
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            | 9 | \centerline {\kern\ht0 \pdfsave\pdfrotate{90}\rlap{\box0}\pdfrestore}
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            | 10 | \caption/f Expected realization of signal digitalisation unit.
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            | 11 | \endinsert
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            | 13 | \sec Required parameters
 | 6 | \sec Required parameters
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            | 15 | We require the following technical parameters in order to overcome the existing digitization units solutions. Primarily, we need a wide a dynamical range and a high third-order intercept point (IP3\glos{IP3}{Third-order intercept point}). The receiver must accept signals with the wide dynamics because a typical radioastronomical signal is a weak signal covered by a strong man-made noise or other undesired noises as lighting, Sun emissions, etc.
 | 8 | We require the following technical parameters in order to overcome the existing digitization units solutions. Primarily, we need a wide a dynamical range and a high third-order intercept point (IP3\glos{IP3}{Third-order intercept point}). The receiver must accept signals with the wide dynamics because a typical radioastronomical signal is a weak signal covered by a strong man-made noise or other undesired noises as lighting, Sun emissions, etc.
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            | 57 | This design ensures that all system devices have access to the defined phase and the known frequency.
 | 50 | This design ensures that all system devices have access to the defined phase and the known frequency.
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            | 59 | \sec System description
 | 52 | \sec System description
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            | 61 | This section deals with the description of the trial version based on Xilinx ML605 development board, see Figure~\ref[ML605-development-board], available at the workplace. This FPGA parameters are more than sufficient of what we need for the fast data acquisition system being developed.
 | 54 | This section deals with the description of the trial version based on Xilinx ML605 development board, see Figure~\ref[ML605-development-board], available at the workplace. This FPGA parameters are more than sufficient of what we need for the fast data acquisition system being developed. Expected system configuration is shown in Figure~\ref[expected-block-schematic]. The system consist antennas equipped by 
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            | - |   | 56 | %% dopsat celkovy popis systemu.
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            | - |   | 57 |  
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            | - |   | 58 | \midinsert
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            | - |   | 59 | \clabel[expected-block-schematic]{Expected system block schematic}
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            | - |   | 60 | \picw=\pdfpagewidth \setbox0=\hbox{\inspic ./img/Coherent_UHF_SDR_receiver.png }
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            | - |   | 61 | \par\nobreak \vskip\wd0 \vskip-\ht0
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            | - |   | 62 | \centerline {\kern\ht0 \pdfsave\pdfrotate{90}\rlap{\box0}\pdfrestore}
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            | - |   | 63 | \caption/f Expected realization of signal digitalisation unit.
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            | - |   | 64 | \endinsert
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            | 63 | \secc Frequency synthesis
 | 67 | \secc Frequency synthesis
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            | 64 |  
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            | 65 | We have used a centralized topology as a basis for frequency synthesis. One precise high-frequency and low-jitter digital oscillator (GPSDO\glos{GPSDO}{GPS disciplined oscillator}) has been used \cite[MLAB-GPSDO]. The other working frequencies have been derived from it by the division of its signal. This central oscillator has a software defined GPS\glos{GPS}{Global Positioning System}  disciplined control loop for frequency stabilization.\fnote{SDGPSDO design has been developed in parallel to this diploma project as a related project, but it is not explicitly required by the thesis itself and thus it is described in a separate document.}
 | 69 | We have used a centralized topology as a basis for frequency synthesis. One precise high-frequency and low-jitter digital oscillator (GPSDO\glos{GPSDO}{GPS disciplined oscillator}) has been used \cite[MLAB-GPSDO]. The other working frequencies have been derived from it by the division of its signal. This central oscillator has a software defined GPS\glos{GPS}{Global Positioning System}  disciplined control loop for frequency stabilization.\fnote{SDGPSDO design has been developed in parallel to this diploma project as a related project, but it is not explicitly required by the thesis itself and thus it is described in a separate document.}
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            | 66 | We have used new methods of software frequency monitoring and compensation in order to meet modern requirements on the radioastronomy equipment, which needs the precise frequency and phase stability over a wide baseline scales for effective radioastronomy imaging.
 | 70 | We have used new methods of software frequency monitoring and compensation in order to meet modern requirements on the radioastronomy equipment, which needs the precise frequency and phase stability over a wide baseline scales for effective radioastronomy imaging.
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