GPS-WAAS Receiver

Product catalog summary

Overview: The document details the specifications and features of the GPS-WAAS receiver from Genesys Aerosystems, designed for LPV approaches. It highlights the receiver's lightweight, compact design, and easy installation options.

Specifications:

GPS Type: C/A code Sensor with WAAS capability.
Conformity: Meets DO-229D, DO-254 Level-B, DO-178B Level-B, DO-160E, ARINC 743A-4 standards.
Certification: TSO-C145b Class Beta 3 for LPV.
Frequency: 1575.42 MHz.
Channels: 15 total (12 GPS, 3 WAAS).
Architecture: Digital Signal Processor with FPGA and RF Front-end.
Measurement Accuracy: Receiver noise per DO-229D.
Time Synchronization: 100 ns, synchronized to GPS or UTC.
Sensitivity: Acquisition at -136 dBm, Tracking at -140 dBm.
Update Rate: 5 Hz.
Dynamics: Speed, acceleration, and jerk per DO-229D requirements.
Alert: Data available as per DO-229D.
Integrity Monitoring: SBAS integrity, FD and FDE RAIM, Predictive RAIM.
BITE: Power-on Self Test and Online BITE.
Communication: RS-232 with one host port and one maintenance port at 19.2 kbps.
Software Upgrade: Field upgradeable.
DO-160E Qualification: [(F2)V]BBBRXWXSFSZZAZ[ZC][YL]M[A3J33]XXAC.
MTBF: 40,000 hrs (MIL-HDBK 217).
COM Ports: RS232, 19,200 bps.
Main Connector Type: MIL-C 38999 Souriau PN: 8D0C-13F35PN.
Antenna Connector Type: Amphenol TNC.
Thermal Protection: Internal thermal regulation and monitoring.
Input Voltage: Nominal 14 to 28V, dual bus, with spikes to 80V and minimum down to 10V for 30 seconds.
Size: 1.4”H x 2.6”W x 4.0”D.
Weight: 0.95 lbs.
Enclosure: Machined 6061-T6 aluminum, black anodized finish.

Key Features:

Utilizes GPS Satellite Constellation and SBAS like WAAS or EGNOS for enhanced precision.
Computes Position, Velocity, and Precise Time (PVT) of aircraft.
Includes Receiver Autonomous Integrity Monitoring (RAIM) for satellite failure detection and exclusion.
Designed for primary navigation receiver for enroute and approach guidance.

Contact Information: Genesys Aerosystems, One S-TEC Way, Municipal Airport, Mineral Wells, TX 76067 USA. Phone: 1-817-215-7600. Website: genesys-aerosystems.com

Catalog excerpts

GPS-WAAS Receiver Latest technology Easy installation GPS-WAAS Receiver Meets requirements for primary navigation receiver for enroute and approach guidance Latest Technology: TSO-C145b BETA 3 for LPV approaches. Lightweight: Less than 1.0 lb. Compact: 1.4”H x 2.6”W x 4.0”D. Easy installation: Stand alone or display integrated. Greater precision The GPS-WAAS receiver from Genesys Aerosystems utilizes the signals coming from Global Positioning System (GPS) Satellite Constellation and Satellite-Based Augmentation System (SBAS) such as WAAS or EGNOS. The primary function of the unit is to compute the Position, Velocity of an aircraft, and the Precise Time (PVT). It also computes the integrity of the PVT from the SBAS signal, if available. The GPS detects and excludes failed satellites (FD/FDE) using Receiver Autonomous Integrity Monitoring (RAIM) algorithm, whenever there are enough number of satellites, regardless of SBAS availabili

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Copyright © 2014 Genesys Aerosystems. All rights reserved. GPS-WAAS Receiver A Global Positioning Receiver (GPS) combined with the unparalleled accuracy and integrity monitoring of Wide Area Augmentation System (WAAS) GPS-WAAS Specifications GPS Type: C/A code Sensor with WAAS capability Conformity: No. of Channels: Total: 15 (GPS: 12 WAAS: 3) Architecture: Digital Signal Processor with FPGA and RF Front-end Measurement Accuracy: Receiver noise per DO-229D Time: Update Rate: Speed, acceleration and jerk per DO-229D requirements for en-route, terminal, non-precision approach and precision approach...

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GPS-WAAS Receiver

GPS-WAAS Receiver

Catalog excerpts

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