GB/T 29081-2012
ActiveModal analysis for spacecraft
航天器模态计算方法
Application Summary AI generated
This standard specifies the methods for calculating the modal parameters (natural frequencies, mode shapes, and damping) of spacecraft structures. It is applied in the aerospace industry during the design, analysis, and ground vibration testing of satellites, launch vehicles, and other spacecraft to ensure structural integrity and dynamic compatibility with launch loads.
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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.