本文件规定了空间控制系统仿真的要求，包括目标、架构和程序等。本文件适用于控制系统开发的四个阶段，包括概念设计、详细设计、原型和集成系统。 本文件中所指的控制系统是指空间系统（包括运载火箭、卫星和宇宙飞船等）的制导、导航和控制飞行控制系统（GNC）。本文件规定了飞行控制系统仿真的最低要求，并为工程师提供了控制系统开发各阶段仿真内容的指导。这些需求本质上是通用的，因为它们广泛适用于所有类型的仿真。 项目特定标准、要求和手册等中阐述了要求的实施细节。

This document establishes the requirements for simulation of the space control system, including the objective, architecture and procedure, etc. This document is applicable to four phases of control system development, including conceptual design, detailed design, prototype and integrated system. The control system referred to in this document is the flight control system for guidance, navigation and control (GNC) of space systems which include launch vehicle, satellite and spaceship, etc. This document establishes a minimum set of requirements for simulation of the flight control system, and provides guidance to engineers on what to simulate in each phase of control system development. The requirements are generic in nature because of their broad applicability to all types of simulations. Implementation details of the requirements are addressed in project-specific standards, requirements, and handbooks, etc.