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GB/T 45435-2025Technical requirements and test methods of BeiDou airborne equipment for aviation supplemental navigation (English PDF)

航空辅助导航北斗机载设备技术要求和测试方法

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Issued by

SAMR; SAC

Level / Type

National · Recommended

Issue date

March 28, 2025

Implementation date

March 28, 2025

Scope

GB/T 45435-2025 is the English-translated version of 航空辅助导航北斗机载设备技术要求和测试方法.

GB/T 45435-2025 is the Chinese national standard covering a BeiDou B1C receiver on a transport or general aviation aircraft for en-route navigation — the system composition, the functional, performance, interface and reliability requirements, the test environment and the test items that check them, the receiving signal and interference conditions the receiver has to work through, the positioning accuracy analysis, the tropospheric correction, and the receiver autonomous integrity monitoring that tells the crew when a satellite has gone bad. BeiDou is supplemental here, not the primary means of navigation, and the failure condition categories the equipment is designed against follow from that. First edition, under the Equipment Development Department of the Central Military Commission. In force from 28 March 2025. Issued on 28 March 2025, it has been in force since 28 March 2025.

Document preview — GB/T 45435-2025

National Standard of the People's Republic of China

ICS
75.010
Classification
E 07

Issued by: State Administration for Market Regulation; Standardization Administration of the PRC

Contents

  • PrefaceIII
  • IntroductionIV
  • 1 Scope1
  • 2 Normative references1
  • 3 Terms, definitions and abbreviations1
  • 3.1 Terms and Definitions1
  • 3.2 Abbreviations2
  • 4 System composition2
  • 5 Requirement3
  • 5.1 Functional Requirements3
  • 5.2 Performance requirements3
  • 5.3 Interface Requirements5
  • 5.4 Reliability5
  • 6 Test Methods5
  • 6.1 Test Environment5
  • 6.2 Test equipment6
  • 6.3 Test Item6
  • 6.4 Functional Testing7
  • 6.5 Performance Testing9
  • 6.6 Interface Testing21
  • 6.7 Reliability Test21
  • Appendix A (Normative) Standard receiving signal and interference environment22
  • Appendix B (Normative) Positioning Accuracy Analysis Method26
  • Appendix C (Normative) General Least Squares Solution and Weights in the Tropospheric Correction Algorithm27
  • Appendix D (Normative) Receiver Autonomous Integrity Method31
  • Reference33

Foreword

This document is in accordance with the provisions of GB/T 1.1-2020 "Guidelines for standardization work Part 1: Structure and drafting rules for standardization documents" Drafting.

Please note that some of the contents of this document may involve patents. The issuing organization of this document does not assume the responsibility for identifying patents.

This document was proposed by the Equipment Development Department of the Central Military Commission.

This document is under the jurisdiction of the National Satellite Navigation Standardization Technical Committee (SAC/TC544).

This document was drafted by: Aerospace Star Technology Co., Ltd., COMAC Beijing Civil Aircraft Technology Research Center, Civil Aviation University of China, China Satellite Navigation Engineering Center, China Institute of Aerospace Standardization.

The main drafters of this document are: Zhou Zhonghua, Yue Fuzhan, Zhang Zhan, Ma Zhenyang, Liu Ying, Li Zeming, Jiang Kexin, Meng Bin, Li Shenyang, Li Tieshuai, Jin, Z.-Wei, Wang, W.-J., Wang, P., and Zhu, B.

Introduction

Beidou airborne equipment for aviation-aided navigation is based on the use of Beidou satellite navigation system by civil aviation industry users in transport aircraft and general aviation aircraft.

It is an airborne dedicated terminal used by the target aircraft in the en-route phase to meet the actual application needs of the B1C frequency point for auxiliary navigation.

The BeiDou airborne equipment specified in this document is expected to provide position/velocity/time (PVT) information to other airborne terminal equipment.

A failure that causes erroneous information is a minor failure state, and a loss of function is a failure state with no safety impact.

Beidou airborne navigation equipment refers to the relevant technical standards of China's civil aviation. Generally, Beidou airborne equipment is divided into two types.

Beta equipment and Gamma equipment, of which Beta equipment consists of independent Beidou airborne equipment, which is expected to be other terminal The terminal device provides information such as position/speed/time (PVT). The error information caused by the failure of Beta devices is a minor failure.

Gamma equipment consists of Beidou airborne equipment and display and control devices, and has route guidance For devices with navigation and display functions, there is no standard minimum failure state category for Gamma devices. Record its functions when designing the device.

Failure condition categories of loss and malfunction.

In order to maintain the compliance of BeiDou airborne equipment with relevant civil aviation standards, the functions of BeiDou airborne equipment in this document are as follows.

The energy and performance requirements are consistent with Beta equipment and are suitable for use on civil aircraft.

Technical requirements for Beidou airborne equipment for aviation-aided navigation and test methods

1 Scope

This document specifies the technical requirements for BeiDou airborne equipment for aviation assisted navigation using BeiDou B1C signals and describes the corresponding tests. method.

This document applies to the development, production, testing and acceptance of Beidou airborne equipment for aviation assisted navigation (hereinafter referred to as Beidou airborne equipment).

2 Normative references

GB/T 5080.7

GB/T 39267

GB/T 39413

GB/T 39414.1-2020

3 Terms, definitions and abbreviations

3.1 Terms and Definitions

The terms and definitions defined in GB/T 39267 and the following apply to this document.

3.1.1 Alarm time timetoalert

The time from when the fault is located to when the device issues an alarm.

[Source. GB/T 42833-2023, 3.1.22]

3.1.2 Positioning failure

The difference between the true position and the calculated position exceeds the corresponding horizontal protection level.

3.1.3

The radius of the circular horizontal area centered on the true position that contains the horizontal positioning position with 95% probability.

3.1.4

When the fault detection and elimination function is available, the radius of the circle centered on the true position that meets the requirements of missed alarms and failure elimination.

......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 33 pages — is available in the English PDF.

Referenced standards

Editions of GB/T 45435

EditionTitleRevisionStatus
GB/T 45435-2025Technical requirements and test methods of BeiDou airborneequipment for aviation supplemental navigationcurrent editionCurrent

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