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GB/T 40698-2021: General requirements for aerospace control system engineering
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| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | Status | PDF |
| GB/T 40698-2021 | English | 369 |
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General requirements for aerospace control system engineering
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GB/T 40698-2021
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Basic data | Standard ID | GB/T 40698-2021 (GB/T40698-2021) | | Description (Translated English) | General requirements for aerospace control system engineering | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V73 | | Word Count Estimation | 20,220 | | Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration | GB/T 40698-2021: General requirements for aerospace control system engineering---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.
General requirements for aerospace control system engineering
ICS 49.020
CCSV73
National Standards of People's Republic of China
General requirements for aerospace control system engineering
Released on 2021-10-11
2022-05-01 implementation
State Administration for Market Regulation
Issued by the National Standardization Management Committee
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 of Standardization Documents"
Drafting.
Please note that some of the contents of this document may involve patents. The issuing agency of this document is not responsible for identifying patents.
This document was proposed and managed by the National Aerospace Technology and Application Standardization Technical Committee (SAC/TC425).
Drafting organizations of this document. Beijing Institute of Aerospace Automatic Control, China Institute of Aerospace Standardization.
The main drafters of this document. Hu Haifeng, Liu Jiarun, Xiao Lihong, Zhang Jun, Zhang Yashun, Xu Guoqiang, Han Lijun, Wang Guanghui, Wang Wei, Sun Zhaogen,
Song Yishu.
General requirements for aerospace control system engineering
1 Scope
This document specifies the aerospace control system engineering technical activities (requirements definition, analysis, design, production, verification and validation, operation, maintenance and
Disposal) general requirements and process requirements.
This document applies to the design, production, verification and use of spacecraft and launch vehicle control systems.
2 Normative references
The content of the following documents constitutes an indispensable clause of this document through normative references in the text. Among them, dated quotations
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 8566 Information Technology Software Life Cycle Process
GB/T 9414.9 Maintainability Part 9.Maintenance and Maintenance Support
GB/T 22032 System Engineering System Life Cycle Process
GB/T 32295 Design Requirements for Surplus Propellant Emissions of Launch Vehicles
GB/T 32297 Space Control System Simulation Requirements
GB/T 32423 System and Software Engineering Verification and Confirmation
GB/T 32451 Aerospace Project Management
GB/T 34513 Space debris mitigation requirements
GB/T 38194 Operational Debris Mitigation Design Requirements for Launch Vehicles
3 Terms and definitions
The following terms and definitions apply to this document.
3.1
Controlcomponent
In order to achieve the control goal, a part or all of the components used in the control system.
3.2
Controller
A control component that enables the controlled object to have specific control performance.
3.3
Sensor
A device that measures the state of the controlled object and inputs it to the controller.
3.4
Actuator
According to the instructions of the controller, the components that control the required force or torque are produced.
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