GB/T 45736-2025
ActiveStable operation requirements for spacecraft attitude and orbit control system
航天器姿态和轨道控制系统稳定运行要求
Application Summary AI generated
This standard specifies the stability criteria, performance indicators, and testing methods for the attitude and orbit control systems of spacecraft during their operational phase. It is applied in the design, verification, and in-orbit management of satellites, space probes, and other space vehicles to ensure precise pointing, orbital maintenance, and safe maneuvering. The standard is primarily used by aerospace engineers and mission operators to validate system reliability and fault tolerance under nominal and contingency conditions.
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Transparency note: The application summary and key sentences on this page were automatically generated by AI from the standard's original text. This content has not been human-verified and should not be used for compliance or regulatory purposes. Always refer to the official standard document from the issuing authority.