Garmin GTX 23 Marine RADAR User Manual


 
190-00906-01 GTX 23 Installation Manual
Rev. C Page 1-4
1.5 Mutual Suppression Pulses
Other equipment on board the aircraft may transmit in the same frequency band as the transponder. DME,
TCAS, or another transponder are examples of equipment that operate in the same frequency band. Mutual
suppression is a synchronous pulse that is sent to the other equipment to suppress transmission of a
competing transmitter for the duration of the transmission. The transponder transmission is suppressed by
an external source, and other equipment on board that transmit in the same frequency band are suppressed
by the GTX 23 transponder. This feature is designed to limit mutual interference.
1.6 Interface Summary
The GTX 23 provides the following interface connections via the rear connector. See Section 4 and
Appendix C for connection details.
External IDENT input
External STBY input (useful for dual transponder installations)
External mutual suppression pulse input/output
Aircraft power input (14/28 Vdc)
RS-232 input #1 connection for altitude and unit control data
RS-232 output #1 connection for TIS and unit status
RS-232 input #2 connection for GPS data for ADS-B
Supports Comm-A and Comm-B protocol
ARINC 429 outputs for TIS data
The GTX 23 supports the following list of Comm-B Definition Subfield (BDS) registers:
BDS (0,0) Air Initiated Comm-B (AICB)
BDS (1,0) Data Link Capability Report
BDS (1,7) Common Usage Ground Initiated Comm-B (GICB) Capability Report
BDS (1,8) Mode S Specific Services GICB Capability Report
BDS (1,9) Mode S Specific Services GICB Capability Report
BDS (1,D) Mode S Specific Services Protocols (MSP) Capability Report
BDS (2,0) Aircraft Identification
BDS (4,0) Selected Vertical Intention
BDS (5,0) Track and Turn Report
BDS (6,0) Heading and Speed Report
BDS (0,6) Extended Squitter surface Position
BDS (0,5) Extended Squitter Airborne Position
BDS (0,8) Extended Squitter Aircraft Identification and Category
BDS (0,9) Extended Squitter Airborne Velocity – Subtypes 1 and 3
BDS (0,A) Extended Squitter Event Driven Data
BDS (6,1) Emergency/Priority Status
BDS (6,5) Aircraft operational Status