A Method for On-orbit Vibration Analysis of Spaceborne Antenna with Cable Net Reflector
A technology of cable-net reflectors and space-borne antennas, applied to instruments, design optimization/simulation, calculations, etc., can solve problems such as time-consuming and labor-consuming, low efficiency, and poor connection of analysis models, so as to avoid repetitive operations and realize The effect of automatic transmission and simplified geometric description
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[0049] In order to make the object, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the examples. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0050] The application principle of the present invention will be described in detail below in conjunction with the accompanying drawings.
[0051] Such as figure 1 As shown, the on-orbit vibration analysis method of the cable net reflector spaceborne antenna of the embodiment of the present invention comprises the following steps:
[0052] S101: Inductively decompose the cable net reflector spaceborne antenna into basic parts with certain functions such as surrounding trusses, cable nets, and reflective wire mesh;
[0053] S102: Describe the geometric characteristics of each part and extract the geometric information of ...
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