Patent GB-1437298-A (GB)
Title: Means for synchronizing an antenna with a digital data display
IPC: G01S7/12
Filed: 1974-11-27
Abstract: 1437298 Pulse radar BENDIX CORP 27 Nov 1974 [18 Dec 1973] 51455/74 Heading H4D A radar digital data display system which has scanning aerial means for emitting radar signals and for receiving radar return signals resulting therefrom also has a memory for storing said return signals in digitized form. The system features means for generating a monitoring signal when the aerial scans through a predetermined position, counting means for counting signals related to the movement in scanning of the aerial whereby said counting means contains a number which ideally is related to the position of the aerial, and means for setting said counting means to a predetermined number in response to the monitoring signal. The system has particular application in arrangements similar to those described in Specifications 1,361,156 and 1,398,506 when using a mechanically scanned aerial. The aerial position number is used in setting up the display of the digitized radar return signals, and the system provides means for periodically making any correction that may be necessary. As described, an aerial 44 is oscillated in azimuth about a central axis or boresight, moving first in a clockwise direction, and then in a counterclockwise direction. Azimuth memory stepping pulses, having a rate which is related to the rate of the aerial azimuth drive pulses are applied via a terminal 10 to first inputs of AND gates 12, 14. When the gate 12 is enabled by a signal on a line 18a to its second input, its output causes an azimuth memory 16 to count upwards (corresponding to aerial motion in a clockwise direction) until a final count is reached, when a signal is given on a line 16c to an aerial sweep control 18, which then deenergizes the line 18a and gives an output on a line 18b, thus enabling the gate 14. The pulses from the terminal 10 then cause the memory 16 to count downwards (corresponding to aerial motion in a counter-clockwise direction) until an initial count is reached, when the cycle recurs. On the downward count the signal on the line 18b also constitutes a first input to an AND gate 48, which receives a second input from a sensor 46 as the aerial scans through the boresight. Output from the gate 48 sets the azimuth memory 16 to a predetermined count (preferably in the middle of its total count) if another count has been reached therein. In a display arrangement suitable for use with the system a circulating memory has a bit capacity for storing an integral number of words, usually the number of words required for a complete scan through an associated display unit or cathode-ray tube. Bits circulate through the memory at a data rate related to a predetermined first pulse frequency signal generated by a coherent control signal generator which also generates a coherent second pulse signal after each group of first signals equal to the number of bits in a word and also generates a coherent third pulse signal after each group of first signals equal to the bit capacity of the memory. When the memory is to be updated, a pulse of the said third signal is applied at a terminal 20, thus enabling a bank of gates 22 to enter the number instantaneously contained in the azimuth memory 16 into an azimuth locater 26. The azimuth locater is also a counter which counts only in a down direction toward zero. Upon reaching zero the azimuth locater generates an output on a line 26a to thus trigger an update enable generator 28 to generate an update signal which permits a word previously contained in an input buffer means to be entered into a proper place in the memory. This is accomplished by counting down the azimuth locater 26 by the pulses at a terminal 24, these pulses being the second pulsed signal which, as was previously explained, is generated after each group of first signals equal to the number of bits in a word. Azimuth drive pulses (ADP) are applied at a terminal 30 which communicates with an azimuth drive 90 degrees device 32. The drive 32 is triggered by the rising edge of the azimuth drive pulses to create a 90 degree phase shift of signals applied thereto. The azimuth drive pulses divided by two (ADP/2) are impressed at a terminal 38 and pass through an AND gate 40, if enabled, and an exclusive-OR gate 42 to the azimuth drive 32. The gate 40 is suitably controlled by a standby switch 36 which in the position shown connects a source of voltage, not shown, to one input of the AND gate 40, thus permitting the ADP/2 signal to pass therethrough. In the alternate position, the standby position, a switch 36 causes gate 40 to close. It will also be noted that the line 18b is connected to the second input of the exclusive- OR gate 42. It will be remembered that this line is energized when the azimuth memory 16 is counting down, corresponding to counterclockwise rotation of the aerial 44. The exclusive-OR gate 42 thus has the capability of inverting the ADP/2 signal applied as its second input when the line 18b is energized or passing the ADP/2 signal directly when the line 18b is unenergized. Also note that the ADP/2 signal is applied directly to aerial drive circuits 44c of the aerial 44 through a line 44b, while the output from the aerial drive 90 degrees device 32 is also applied thereto through a line 44a. The aerial drive circuits are arranged in a known manner to drive the aerial in a counter-clockwise direction when the signals on the line 44a lead the signals on the line 44b by 90 degrees and to drive the aerial in a clockwise direction when the signals on the line 44a lag the signals on the line 44b by 90 degrees. The ADP/2 signal may be obtained by dividing the ADP signal in half using a flip-flop. The signal from the boresight sensor 46 is also applied to a boresight monitor 50 which in response thereto generates a signal which is applied to the update enable generator 28. This signal from the boresight monitor is a relatively long signal which, so long as it is generated, permits the update enable generator 28 to continually update the system memory. However, should the boresight sensor 46 fail to generate its output over a predetermined period of time the update enable generator 28 will be disabled so that the memory cannot be further updated. When the update enable generator 28 generates its update signal it simultaneously generates a signal which is applied to a video blank generator 54 which in response thereto blanks the range line then being generated on the cathode-ray tube. Since updating of the words in the memory occurs sequentially there normally appears on the cathode-ray tube a blank line which sweeps at a rate related to the sweep rate of the aerial 44. This sweeping line indicates that the system is synchronized and that updating of the memory is continually occurring. Disappearance of this line will indicate to the observer that updating of the memory is no longer occurring.