Research Article
Application of Stewart Platform in the Low-Frequency Vibration Characteristic Test of Space Truss Deployable Antenna on Satellite
Table 1
Input conditions for low-frequency vibration test.
| Direction | Frequency (Hz) | Magnitude |
| | 0.4 ~ 1.8 | 0.04~0.45 g | 1.8 ~ 6 | 0.45 g | 6 ~ 8 | 0.45~0.65 g | | 0.4 ~ 2.1 | 0.1 ~ 0.33 g | 2.1 ~ 8 Hz | 0.33 g | | 0.8 ~ 5 | 0.2 g | Scanning rate | 0.05 Hz/s |
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