GB/T 42042-2022 English PDF

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GB/T 42042-2022: Space station coordinate system
Status: Valid

Standard ID	USD	BUY PDF	Lead-Days	Standard Title (Description)	Status
GB/T 42042-2022	889	Add to Cart	6 days	Space station coordinate system	Valid

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Basic data

Standard ID: GB/T 42042-2022 (GB/T42042-2022)
Description (Translated English): Space station coordinate system
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V70
Classification of International Standard: 49.020
Word Count Estimation: 42,434
Date of Issue: 2022-10-12
Date of Implementation: 2022-10-12
Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration

GB/T 42042-2022: Space station coordinate system

---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
Space station coordinate system ICS 49.020 CCSV70 National Standards of People's Republic of China space station coordinate system Released on 2022-10-12 2022-10-12 implementation State Administration for Market Regulation Released by the National Standardization Management Committee

table of contents

Preface I 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 quadrants and coding 1 4.1 Spacecraft quadrant 1 4.2 Coordinate system coding 3 5 Space Station Coordinate System Definition 3 5.1 Definition of sky and core module coordinate system 3 5.2 Definition of coordinate system of Wentian experimental cabin 4 5.3 Definition of Mengtian experimental cabin coordinate system 4 5.4 Definition of assembly coordinate system 5 5.5 Definition of manipulator coordinate system 5 5.6 Space application coordinate system definition 5 5.7 Other coordinate systems 5 6 Coordinate system conversion 5 Appendix A (Normative) Space Station Coordinate System Transformation 33 Reference 38

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 contents of this document may refer to patents. The issuing agency of this document assumes no responsibility for identifying patents. This document is under the jurisdiction of the National Manned Spaceflight Standardization Technical Committee (SAC/TC570). This document is drafted by. Beijing Space Vehicle Overall Design Department, Beijing Institute of Space Science and Technology Information, Space Application Institute of Chinese Academy of Sciences Engineering and Technology Center, Shanghai Institute of Aerospace Systems Engineering. The main drafters of this document. Su Liang, Diao Changkun, Jin Weiwei, Zhu Guangchen, Zhang Qiao, Zhou Qiang, Wang Hao, Zhao Shuo, Wang Yubai, Wang Wei, Gao Hui, You Jin, Sunan, Zhang Peng, Zhou Fengxiang, Zhao Hui, Zhu Xin, Wang Youyu, Yin Lina, Sun Xiaozhu, Li Lichun, Lou Qiao, Zhao Zhenhao. space station coordinate system

1 Scope

This document specifies the numbering of the space station and each cabin, the definition and conversion of quadrant lines, and the main coordinate system. This document is applicable to the engineering development, launch, in-orbit operation, assembly and flight control of the space station.

2 Normative references

The contents of the following documents constitute the essential provisions of this document through normative references in the text. Among them, dated references For documents, only the version corresponding to the date is applicable to this document; for undated reference documents, the latest version (including all amendments) is applicable to this document. GB/T 32296-2015 Commonly used coordinate systems for aerospace vehicles

3 Terms and Definitions

This document does not have terms and definitions that need to be defined.

4 quadrants and coding

4.1 Spacecraft quadrants 4.1.1 Sky and Core Module Quadrant Lines The sky and core module quadrants are the baselines used to characterize the sky and core module. On the aircraft, the four cabin mothers with an opening angle of 90° The line is the quadrant line of the sky and the core cabin. As shown in Figure 1, the sky and the core cabin fly from the rear end of the resource cabin along the longitudinal axis (the symmetrical longitudinal axis of the sky and the core cabin). Viewed in the row direction, the quadrants in the clockwise direction change to I, II, III, and IV. The quadrants are separated by 90°, and the three-axis stable flight to the ground in orbit I image Limit line to ground. Note. The longitudinal axis of symmetry of the cabin is used to characterize the geometric axis of symmetry of the cabin. coincide. 1) 1) Tianhe Core Module, Wentian Experimental Module and Mengtian Experimental Module are trade names provided by China Manned Space Engineering Office. ......

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