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<br />..: <br /> <br />~. <br /> <br />499 <br /> <br />APRIL 1978 <br /> <br />MELVIN J. SCHROEDER AND GERARD E. KLAZURA <br /> <br />TABLE 1. Characteristics of HIPLEX SWR-75 radars. <br /> <br />does not interfere with the monitoring and recording <br />of the precipitation- data. <br /> <br />3. Calibration and transfer function <br /> <br />Radar and digitizer calibrations are crucial to attain- <br />ing useful data from the DVIP-produced numbers <br />recorded on the magnetic tape. Electronic and sphere <br />calibration procedures are used. Complete system <br />calibration is performed on each of the radars at the <br />beginning and end of each operational season. This <br />calibration consists of a measurement of the effective <br />antenna system gain and also incorporates a pre-, mid- <br />and post-season antenna boresighting, elevation and <br />azimuth error determinations and corrections using <br />solar evaluations. <br />Digitizer calibrations to relate the recorded binarv <br />eight-bit number in each bin to a received power at the <br />radar are made weekly. The DVIP is quite stable, <br />usually not deviating by more than i dB from one week <br />to the next. The DVIP calibration consists basically <br />of injecting RF test signals of specified power levels <br />through the directional cDupler into the receiver. For <br />each DVIP level the test signal and corresponding <br />, digitizer response are recorded (dBm vs DVIP units). <br />Later a polynominal regression analysis of these dBm/ <br />DVIP data is carried out to compute the coefficients <br />of a third-order equation of the form <br /> <br />y= a+bx+cx2+dr, <br /> <br />where x is the DVIP value and y the corresponding <br />estimated dBm value. <br />Daily checks consist of measuring the pulse repetition <br />frequency, average power, transmitter frequency, <br />minimum discernable signal and checking three levels <br />of the DVIP. If the DVIP varies by more than! dBm <br />from the weekly calibration, a complete recalibration <br />is performed. <br />An independent evaluation of the Miles City radar <br />and calibration procedures was carried out by Smith <br />(1977). <br />Recorded data are not range-corrected, but subse- <br />quent data processing introduces the correction. The <br />2.5 dBm log-averaging correction (Lhermitte and <br />Kessler, 1965) and 0.2 dBm finite incremental trunca- <br />tion bias correction (Sirmans, 1972) are also made <br />during the computer processing stage. <br /> <br />4. Data acquisition and flow <br /> <br />a. Data acquisition <br /> <br />Recording of data is accomplished in two modes of <br />operation-surveillance and volume. While in the sur- <br />veillance mode, one 5 min volume scan (3600 in azimuth <br />and 120 in elevation starting at 10 and going in steps <br />of 10) is taken on the hour and 30 min past the hour. <br />The purpose of the surveillance mode is to' detect <br />echoes within 150 km, at which time recording of con- <br /> <br />Peak transmitter power <br />Pulse duration <br />Antenna type <br />Horizontal half-power beam width <br />Vertical half-power beamwidth <br />Effective system gain <br />Wavelength <br />Pulse repetition frequency <br />Receiver noise <br />Receiver <br />Receiver bandwidth <br />Receiver dynamic range <br />System noise figure <br /> <br />250 kW <br />2.0,..s <br />circular parabolic <br />0.90 <br />1.00 <br />43.7* dB <br />5.4cm <br />207/414 pps <br />2 dB <br />logarithmic <br />0.6 MHz <br />80 dB <br /><3 dB <br /> <br />* This figure incorporates all waveguide mismatch and similar <br />losses beyond the directional couplers as well as radome loss. <br /> <br />(1) <br /> <br />tinuous, sequential, 5 min volume scans begins. The <br />antenna azimuth sweep and elevation step sequence are <br />automatically regulated. The sweep rate is controlled <br />by the pulse repetition frequency (PRF) setting and <br />number of pulse samples per averaged return (SA). For <br />HIPLEX the PRF is set at 414 and the SA is set at 32 <br />for a base elevation sweep and 16 for higher elevation <br />sweeps. This translates to a sweep duration (one <br />antenna rotation) of 34 s at 10 elevation and 17 s for <br />the other elevations. The returned signals are digitized <br />and linearly averaged over the range bin interval using <br />rectangular integration techniques. Pulse-to-pulse aver- <br />aging is initiated on the whole azimuth angle (e.g., <br />273.00) and terminates after about 0.70 (e.g., 273.70) <br />in the 10 azimuth recording mode. Each !-km range bin <br />value is determined by adding four t km (in range) <br />samples, dividing by 4, and repeating and accumulating <br />until the number of samples specified by SA is fulfilled <br />at which time the sum is divided by SA to produce the <br />DVIP number. <br />A "blue-sky" elimination feature is wired into the <br />radar hardware so that only records containing at least <br />one radial with bin data above a preset threshold level <br />are recorded. The first and last records of a 'constant <br />elevation sweep are always recorded to maintain <br />antenna sweep history. <br /> <br />b. Description of magnetic tape record <br /> <br />Each magnetic tape record (Fig. 1) consists of 22 <br />frames of housekeeping information (date, time, radar <br />settings, etc.) and four sets of 1) four frames of azimuth <br />and elevation data, 2) 250 frames of averaged-echo <br />range bin data, 3) three frames of project aircraft posi- <br />tions, and 4) three frames of automatic calibration data. <br />Housekeeping information includes a frame for <br />operator's notes which are loaded via a special key- <br />board. This is primarily used to record pertinent infor- <br />mation about project aircraft (i.e., locations, times, <br />seeding, cloud penetrations, etc.). The range delay sett- <br />ing (switch selectable 0-99) is used to specify the range <br />of the first data bin; scan mode inciit.ates whether the <br />