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Database: 365,228(8 Aug 2026)
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GB/T 42577-2023 in English

GB/T 42577-2023 in English

VALID

Definitions and descriptions of BeiDou/global navigation satellite system(GNSS) satellite parameters for high precision applications

  • Issued on:2023-05-23
  • Implemented on:2023-05-23
  • File Format:PDF
  • Delivery:Via email within 5 business days
Price(USD): $430.00
$418.00
Standard No: GB/T 42577-2023
Document status: VALID
Title in English: Definitions and descriptions of BeiDou/global navigation satellite system(GNSS) satellite parameters for high precision applications
Title in Chinese: 北斗/全球卫星导航系统(GNSS)卫星高精度应用参数定义及描述
Language: English
File Format: Electronic (PDF)
Delivery: Via email within 5 business days
Issued on: 2023-05-23
Implemented on: 2023-05-23
Professional Classification: GB-National Standard
Related Keywords: satellite parameters
beidou/global navigation satellite system
key parameters
satellite attitude control
satellite coordinate system inter-frequency clock error
Related Topics: Navigation System
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satellite peak effect
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Definition of Sphericity
The 42nd and 43rd satellites of the Beidou satellite navigation system
43 Beidou satellites
The 42nd and 43rd Beidou satellites
The 42nd and 43rd Beidou navigation satellites
Beidou satellite navigator
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The 42nd and 43rd navigation satellites
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How many Beidou satellites are there now?
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China Beidou Satellite Navigation System Distance () Target
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gb/t 42577-2023

《GB/T 42577-2023北斗/全球卫星导航系统(GNSS)卫星高精度应用参数定义及描述》由TC544(全国北斗卫星导航标准化技术委员会)归口,主管部门为中央军委装备发展部。


Introduction

Analysis of the core content of the standard

This standard systematically defines for the first time six major categories of key parameters of BeiDou/GNSS satellites in high-precision applications:

Parameter categoryTechnical factorsPrecision impact
Basic satellite informationSVN/PRN identification, quality, optical pressure parametersOrbit determination accuracy±2cm
Phase center deviation (PCO)Three-dimensional deviation in mechanical/celestial coordinate systemPositioning accuracy±1mm
Phase Center Variation (PCV)Azimuth/Altitude Correlation Correction ModelAltitude Accuracy±3mm
Equipment Delay DeviationUPD/IFPB/DCB/ISBTime Synchronization±0.1ns

Key Technology Breakthroughs

1. Satellite Attitude Control Modeling

The standard specifies the calculation methods of three attitude modes for the first time:

  • Dynamic Yaw Mode: When the solar altitude angle β≥β₀, the yaw angle ψₘ=arctan(Sₒᵧ/Sₒₓ)
  • Maneuvering Yaw Mode: When β<β₀, piecewise function calculation is used
  • Bias mode: Keep ψₘ=0°

Actual case: When the BEIDOU-3M satellite switches at β=3°, the threshold control of ϕ₀=5° is used to avoid sudden attitude change


Standardized file system

1. Satellite information file format

A hierarchical data structure is adopted. The key fields include:

 +SATEINFO SYSTEM | SVN | COSPAR-ID | PRN SOLARPRESSURE Satellite component 1 shape/orientation/material coefficient-SATEINFO

2. Phase center file specification

ANTEX format enhancement:

  • Add Beidou frequency point identification (C01-B1c, C05-B2a)
  • Supports absolute/relative phase center values
  • Typical data block example:
     START OF FREQUENCY C02 600.00 0.00 1100.00 NORTH/EAST/UP NOAZI 0.00 0.00 0.00... END OF FREQUENCY

Implementation Suggestions

  1. Data update mechanism: It is recommended to check the satellite quality, optical pressure coefficient and other variable parameters every month
  2. Multi-system compatibility: GPS/GLONASS equipment delay needs to be corrected according to the ISB parameters in Appendix E
  3. Accuracy verification: PCV model verification is performed using iGMAS station network data

Typical problem solutions

Problem phenomenonTroubleshooting steps
Elevation deviation>5mm1. Check if the elevation angle interval of the PCV file is 0.5°
2. Verify the definition of the satellite coordinate system
Inter-frequency clock error is inconsistent1. Load the IFPB parameter file
2. Check the inter-frequency phase deviation item in Appendix E

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