Honeywell International Inc. 9PGTPL-100A 사용자 설명서

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MAINTENANCE MANUAL
TPL-100A Processor / Part No. 940-0530-001
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
In the case of a TCAS/ATCRBS interrogation transmission, the TCAS message is 
transmitted from the directional main beam with the exception of the ATCRBS 
suppression pulse (P2) which is transmitted in an omni pattern as shown in Figure 6. 
To create the omni pattern for the ATCRBS suppression pulse, the four signals 
representing the suppression pulse from the MILACAS-FR Processor to the four 
elements of the antenna are of equal phase and amplitude. This results in the omni 
pattern being radiated for the ATCRBS suppression pulse.
NOTE: The P2 pulse for Change 7 units is transmitted with a directional pattern, but 
in a direction opposite the main beam.
ATCRBS Mode A and Mode C transponders in the surrounding airspace (which detect 
an omni suppression beam signal larger in amplitude than the main beam signal) are 
suppressed from replying to the interrogation. The result of the ATCRBS P2 
suppression is to control the effective TCAS interrogation beam width and thus limit 
interference from unwanted ATCRBS receptions. The effective beam width is 
narrowed by increasing the amplitude of the suppression omni pattern output or 
decreasing the amplitude of the main beam pattern output.
During TCAS receptions, each of the four directional antenna elements receives any 
1090-MHz signal that passes by the element. The phasing of these received signals is 
determined by the direction from which the RF energy is received. These signals are 
directed onto the same four cables that connect transmit signals between the 
MILACAS-FR processor and the directional antenna.
Multiple receivers are used in the MILACAS-FR Processor to perform noise 
suppression and pulse shaping on the received signals. Phase detectors in the 
MILACAS-FR Processor then examine the relative phasing of the four signals from the 
antenna and produce an analog voltage that represents the bearing of the intruder 
aircraft that sent the replies.
The main beam pointing angle is redirected in a matter of microseconds, to any of four 
90
°
 pointing positions.
Four coaxial cables with type TNC plugs on the antenna end connect the directional 
antenna to the MILACAS-FR Processor.
Each of the four ports of the directional antenna contains a resistor located across the 
antenna element to ground. Each of the four resistors is a different value. The 
MILACAS-FR Processor periodically performs a continuity check on the antenna ports 
and to see the correct resistance value (through an A/D converter) if the port is not 
shorted or not open.
The directional antenna is a passive device and does not require aircraft power.
Refer to ANT-81A Directional Antenna Component Maintenance Manual for additional 
information.