BS EN 16603-60-30:2015规定了姿态和轨道控制系统的基线 空间项目要求文件中使用的要求 应用。项目需求文档包含在业务协议中，其中 在任何空间级别上，由双方商定并对其具有约束力 计划，如ECSS-S-ST-00所述。本标准涉及按照以下要求开发的姿态和轨道控制系统: 卫星空间项目的一部分。经典的姿态和轨道控制系统 这里考虑的功能包括:姿态估计机构制导机构控制轨道控制轨道估计，在本文中称为导航，可以是 明确要求在紧急情况下获取并保持安全态度的任务的功能，以及 本标准不包括以下任务: 功能:实时机载弹道制导和控制实时机载相对位置估计和控制这类任务的例子有交会、编队飞行、运载火箭 以及星际飞行器。尽管本文件不包括上述类型的 它可以作为他们的参考文件。本标准可针对某一产品的特定特性和限制进行定制 符合ECSS-S-ST-00的太空项目。参考交叉参考:EN 16601-0-0-0-0-01 ECSS-0-0-0-10-10-10-10-10-10-10-ECSS-10-10-3-ECSS-E-E-E-ST-10-10-10-10-10-10-10-10-10-3-10-10-10-ECSS-E-10-E-E-10-E-10-10-10-10-10-10-10-10-10-10-10-10-10-10-10-10-3-10-3-10-3-6-6-3-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6-6 ECS-30-02ECSS-Q-ST-30-02购买时可用的所有当前修订版包括在购买本文件时。

BS EN 16603-60-30:2015 specifies a baseline for the attitude and orbit control system requirements to be used in the Project Requirements Document for space applications.Project requirements documents are included in business agreements, which are agreed between the parties and binding them, at any level of space programmes, as described in ECSS-S-ST-00.This Standard deals with the attitude and orbit control systems developed as part of a satellite space project. The classical attitude and orbit control systems considered here include the following functions:Attitude estimationAttitude guidanceAttitude controlOrbit controlOrbit estimation, called Navigation in this document, can be part of the function for missions which explicitly require this functionAcquisition and maintenance of a safe attitude in emergency cases and return to nominal mission upon commandThe present Standard does not cover missions that include the following functions:Real-time on-board trajectory guidance and controlReal-time on-board relative position estimation and controlExample of such missions are rendezvous, formation flying, launch vehicles and interplanetary vehicles.Although the present document does not cover the above mentioned types of mission, it can be used as a reference document for them.This standard may be tailored for the specific characteristic and constraints of a space project in conformance with ECSS-S-ST-00.Cross References:EN 16601-00-01ECSS-S-ST-00-01EN 16603-10ECSS-E-ST-10EN 16603-10-03ECSS-E-ST-10-03EN 16603-60-10ECSS-E-ST-60-10EN 16603-70-11ECSS-E-ST-70-11EN 16601-00ECSS-S-ST-00EN 16603-10-02ECSS-E-ST-10-02EN 16603-10-06ECSS-E-ST-10-06EN 16603-10-09ECSS-E-ST-10-09EN 16603-70ECSS-E-ST-70EN 16603-70-41ECSS-E-70-41EN 16602-30-02ECSS-Q-ST-30-02All current amendments available at time of purchase are included with the purchase of this document.