Volume 42 Issue 4
Jul.  2012
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ZOU Yuanjie, HAN Zengyao, ZHANG Jin. RESEARCH PROGRESS ON FULL-FREQUENCY PREDICTION TECHNIQUES OF SPACECRAFT'S MECHANICAL ENVIRONMENT[J]. Advances in Mechanics, 2012, 42(4): 445-454. doi: 10.6052/1000-0992-11-075
Citation: ZOU Yuanjie, HAN Zengyao, ZHANG Jin. RESEARCH PROGRESS ON FULL-FREQUENCY PREDICTION TECHNIQUES OF SPACECRAFT'S MECHANICAL ENVIRONMENT[J]. Advances in Mechanics, 2012, 42(4): 445-454. doi: 10.6052/1000-0992-11-075

RESEARCH PROGRESS ON FULL-FREQUENCY PREDICTION TECHNIQUES OF SPACECRAFT'S MECHANICAL ENVIRONMENT

doi: 10.6052/1000-0992-11-075
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  • Corresponding author: ZOU Yuanjie
  • Received Date: 2011-05-26
  • Rev Recd Date: 2011-08-31
  • Publish Date: 2012-07-25
  • The mechanical environment prediction technique of spacecraft is critical to spacecraft system design and structure design, especially to spacecraft for first launch, since it lacks telemetry data from similar spacecraft and thus could only rely on effective prediction means to establish the ground test scheme and related test requirements. No individual analysis method could get accurate prediction results for full-frequency bands currently, because spacecraft at launch experiences full-frequency dynamic loads, which bring about great discrepancy of structure responses at different frequencies. The full-frequency mechanical environment prediction technique is described regarding low-frequency, mid-frequency and high-frequency band, respectively. In the end, according to the requirement of domestic spacecraft engineering, the main research directions are presented for the full-frequency mechanical environment prediction.

     

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