Space systems - Stable operation requirements for spacecraft attitude and orbit control system
This document provides the criteria for stable on-orbit operation of the spacecraft's AOCS. It addresses the factors affecting the spacecraft's on-orbit stability by specifying principles and requirements for establishing the spacecraft AOCS's capability for stable on-orbit operation, which include:
—    principles for judging data validity and the requisite procedures for handling such data;
—    anomaly detection;
—    management of software and hardware failures;
—    safety boundary checks;
—    activation protocols for emergency survival modes.
This document also establishes the functional interface between on-orbit autonomy and ground-based maintenance operations, ensuring that the spacecraft maintains its intended attitude and orbit.
This document is applicable to the attitude and orbit control systems of various types of spacecraft.
| SDO | ISO: International Organization for Standardization |
| Document Number | ISO 16615 |
| Publication Date | Jan. 1, 2025 |
| Language | en - English |
| Page Count | 18 |
| Revision Level | |
| Supercedes | |
| Committee | ISO/TC 20/SC 14 |
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