Trapezoid type small satellite structure suitable for carrying
A technology of satellite structure and form, applied in the field of spacecraft structure, can solve problems such as reducing the volume of the whole satellite, and achieve the effect of reducing weight, simple and convenient connection, and saving space in the satellite
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[0018] In the following, the method for calculating the imaging yaw guidance angle of a stationary satellite according to the present invention will be further described in detail with reference to the accompanying drawings and specific embodiments.
[0019] Such as Figure 1-Figure 2 As shown, in order to meet the space envelope constraint requirements of the carrier fairing, the small satellite structure 1 adopts a ladder-shaped configuration as a whole, and is installed on the cone section of the carrier rocket support cabin through a three-point connection. The connection point 2 is set Way like Figure 2-Figure 3 Shown.
[0020] In order to maximize the internal layout space of the structure, during the structural design process, no additional force transmission components such as partitions, bulkheads or struts are provided inside the cabin. At the same time, in order to obtain the rigidity of the entire star, in the process of structural design, a method of laying embedded ...
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