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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.
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