AIRBORNE GLOBAL POSITIONING SYSTEM RECEIVER

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-03-1990

Publisher

Aeronautical Radio Inc.

1.0 INTRODUCTION
1.1 Purpose of this Document
1.2 Summary of GPS System Operational Characteristics
1.3 Brief Description of the System
1.4 Interchangeability
1.5 Regulatory Approval
1.6 Reliability
1.7 Testability and Maintainability
2.0 INTERCHANGEABILITY STANDARDS
2.1 Introduction
2.3 Standardized Signaling
2.4 Standard Interwiring
2.5 Power Circuitry
2.6 Environmental Conditions
3.0 GPS SENSOR SYSTEM DESIGN
3.1 General
3.2 System Application
3.3 General System Capabilities
3.4 Specific System Capabilities
4.0 GPS SENSOR DESIGN
4.1 Integrity
4.2 Modes
4.3 System Interfaces
4.4 Sensor Performance (2 MCU Configuration)
5.0 INTEGRATED ANTENNA/PREAMPLIFIER/FILTER DESIGN
5.1 Antenna Requirements
5.2 Preamplifier Assembly Performance
5.3 Antenna/Preamplifier/Filter Requirements
5.4 Physical Characteristics

Describes the characteristics of the Global Positioning System (GPS) sensor portion of a GPS system intended for installation in commercial transport aircraft.

DocumentType	Standard
Pages	42
PublisherName	Aeronautical Radio Inc.
Status	Current

FAA AC 20-165 : 2015	AIRWORTHINESS APPROVAL OF AUTOMATIC DEPENDENT SURVEILLANCE - BROADCAST OUT SYSTEMS
FAA AC 20-172 : 2015	AIRWORTHINESS APPROVAL FOR ADS-B IN SYSTEMS AND APPLICATIONS