Abstract
Frequency shifts often take place in the vibration tests of satellites. This paper focuses on analysis of the causation, the mechanism and the hazard of a frequency shift. Either the nonlinear satellite structure or the dilation of scathe is the main causation of the recoverable frequency shift. The result of the nonlinear dynamic parameter test with the honeycomb sandwich plane corroborates the analysis.
| Original language | English |
|---|---|
| Pages (from-to) | 74-75+80 |
| Journal | Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology |
| Volume | 38 |
| Issue number | 1 |
| State | Published - Jan 2006 |
| Externally published | Yes |
Keywords
- Frequency shift
- Honeycomb sandwich plane
- Vibration
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