GB/T 32297-2015 English PDF

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GB/T 32297-2015: Simulation requirements for space control system
Status: Valid

Standard ID	USD	BUY PDF	Lead-Days	Standard Title (Description)	Status
GB/T 32297-2015	529	Add to Cart	5 days	Simulation requirements for space control system	Valid

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Basic data

Standard ID: GB/T 32297-2015 (GB/T32297-2015)
Description (Translated English): Simulation requirements for space control system
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V73
Classification of International Standard: 49.14
Word Count Estimation: 25,257
Date of Issue: 2015-12-31
Date of Implementation: 2016-07-01
Adopted Standard: ISO 16781-2013, MOD
Regulation (derived from): State Standard Announcement 2015 No.43
Issuing agency(ies): General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China, Standardization Administration of the People's Republic of China
Summary: This standard specifies the purpose, simulation composition and function of the simulation of space flight control system, general requirements of simulation, detailed requirements of simulation at different stages such as conceptual design, detailed design, engineering prototype and system integration. This standard applies to spacecraft control system simulation test, other city simulation test can refer to use.

GB/T 32297-2015: Simulation requirements for space control 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.
Simulation requirements for space control system ICS 49.140 V73 National Standards of People's Republic of China Aerospace Control System Requirements (ISO 16781.2013, Spacesystems- Simulationrequirementsforcontrolsystem, MOD) Issued on. 2015-12-31 2016-07-01 implementation Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China Standardization Administration of China released

Table of Contents

Introduction Ⅲ Introduction Ⅳ 1 Scope 1 2 Terms and definitions 1 3 control system simulation purposes 2 4 control system simulation of components and functions 3 4.1 Control System Simulation consisting of 3 4.2 Mathematical simulation and semi-physical simulation 3 4.3 Control System Design and Control System Simulation correspondence between 4 4.4 Simulation Process 6 5 Simulation General requirements 7 5.1 Overview 7 5.2 system-level requirements 7 5.3 Simulation Model Requirements 7 5.4 Simulation Facility Requirements 8 5.5 simulation carried out in claim 8 5.6 Simulation results analysis requirements 9 5.7 Documentation Requirements 9 6 concept design simulation requirements 11 6.1 Overview 11 6.2 Objective 11 6.3 input 11 6.4 Output 12 6.5 Simulation model requires 12 6.6 Simulation Facility requirements 12 6.7 simulation carried claims 12 7 Detailed design simulation requirements 12 7.1 Overview 12 7.2 Objective 13 13 7.3 Input 13 7.4 Output 7.5 Simulation model requires 13 7.6 Simulation Facility requirements 13 7.7 simulation carried claims 13 8 engineering prototype simulation requirements 14 8.1 Overview 14 8.2 Objective 14 14 8.3 Input 15 8.4 Output 8.5 Simulation model requires 15 8.6 Simulation Facility requirements 15 8.7 simulation carried claims 15 9 integrated simulation system requirements 15 9.1 Overview 15 9.2 Objective 16 9.3 Input 16 16 9.4 Output 9.5 Simulation model requires 17 9.6 Simulation Facility requirements 17 9.7 simulation carried claims 17 Appendix A (informative) This standard and ISO 16781.2013 Chapter 18 Article ID control list Annex B (informative) in this standard process control system design and development phase of the correspondence between the practice aerospace systems 19

Foreword

This standard was drafted in accordance with GB/T 1.1-2009 given rules. This standard uses redrafted Law Amendment uses ISO 16781.2013 "Space Control System Simulation System Requirements." The presence of structural changes compared to 2013, listed in Appendix A of this standard and ISO 16781.. This standard and ISO 16781 clauses 2013 No control list. This standard and ISO 16781.2013 technical differences and their reasons are as follows. --- Modify the "1" or make statements simple, easy to use as the executive summary, in order to meet the requirements of the standard system and write; --- Revised ISO 16781.2013 in Table 7 "should be recognized simulation models and facilities have been checking" and "should have been confirmed Simulation Facility After verification, "prepared for the standard in Table 6" should be recognized simulation models and facilities have been checking "to adapt our technology Article Members and practices. This standard made the following editorial changes. --- In order to meet our national standards system and language habits, the standard name will be changed to "space control system simulation requirements"; --- The abbreviations used instead of Chinese Interpretation; --- Remove the ISO 16781.2013 Annex A (Informative Appendix) "ISO 14300 and ISO 16781 in all stages of the correspondence system"; --- Remove the ISO 16781. Annex B (informative) "2013 control system simulation and design process for each of the chapters listed in the table Relationship"; --- Added Appendix A (informative) "This standard and ISO 16781.2013 Number of reg control list"; --- Added Appendix B (informative) "this standard process control system design and development phase corresponds to the practice of aerospace systems relationship". The standard proposed by China Aerospace Science and Technology Corporation. This standard by the National Aerospace Technology and Application of Standardization Technical Committee (SAC/TC425) centralized. This standard was drafted. Beijing Aerospace Automatic Control Institute. The main drafters of this standard. Tian Haitao, Wang Kuaixia, Liu Jiarun, Zheng quasi-total, He Yong, Yu Chunmei, Zhang Guowei, Tan Yun, Zou Ying, Chen Shuguang.

Introduction

On the spacecraft control system as an important subsystem, can protect the spacecraft attitude stabilization, it required along Orbital flight. Control system simulation can test the system performance, system design verification, fault simulation and implement countermeasures and other tasks. for The simulation of the control system for effective, China's aerospace control system simulation test requests, clear methods and processes, and Launch vehicles, satellites, manned spacecraft and other spacecraft development process has been successfully tested and applied. This standard will aerospace control system simulation The true test of conduct play an effective role in guiding. Aerospace Control System Requirements

1 Scope

This standard specifies the spacecraft control system simulation purposes, the simulation components and functions, as well as general requirements for simulation concept design, detailed design, Detailed requirements engineering prototype, system integration at different stages of the simulation. This standard applies to the spacecraft control system simulation, simulation can refer to other areas of use.

2 Terms and definitions

The following terms and definitions apply to this document. 2.1 Accuracy accuracy The degree of difference parameter value and its "true value" between. 2.2 Controlsystem control system According to the mission and related information, in accordance with predetermined rules and control requirements, spacecraft flight control organic combination of soft and hard Member system. 2.3 Equivalent device emulator Equivalent devices spacecraft equipment, has the same kind of device input and output interfaces, and similar dynamic behavior. 2.4 Fidelity fidelity The simulation is now level objects of a complex simulation side or the whole state and external behavior. 2.5 HILS hardwareintheloopsimulation The simulation of physical access control systems - Part loop simulation carried out. 2.6 Mathematical simulation mathematicalsimulation All simulation models are implemented using software emulation. 2.7 Real-time simulation of real-timesimulation Real time simulation model of propulsion system to promote the same time simulation. 2.8 Reliability reliability Within a given time interval and the given conditions, the ability to complete the required function. 2.9 Simulation simulation Using a similar or equivalent system to simulate the real system, or make it behave similar to the performance of the real system. ......

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