Butt joint and regulation equipment for solar wings of moonlet
A technology for adjusting equipment and satellites, which is applied in the field of satellite testing, can solve problems such as large loads of satellites and support vehicles, unobstructed adjustment equipment, and high labor intensity of personnel, and achieve the effects of reduced operation steps, large loads, and low cost
Active Publication Date: 2014-11-19
AEROSPACE DONGFANGHONG SATELLITE
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Problems solved by technology
Although this method can meet the docking requirements, it has a low safety factor, low adjustment accuracy, and high labor intensity.
[0004] At the same time, when improving the existing method, there are still some constraints: for example, the docking height of the whole satellite is limited, and the height of the satellite support vehicle must be less than 70mm during adjustment; the load of the satellite and the support vehicle is large, and the mass is about 1400kg; Due to size and width restrictions, the small satellite solar wing will mark the position on the ground when it is docked, and the adjustment equipment cannot block the position mark on the ground; the span limit, the fulcrum of the adjustment equipment must have a certain distance to ensure the stability requirements when the satellite solar wing is docked ; In addition, it is necessary to realize a certain amount of adjustment to the six degrees of freedom of the whole star
Method used
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Embodiment Construction
[0016] The present invention will be further described below in conjunction with the drawings.
[0017] In this embodiment, the structure of the small satellite solar wing docking adjustment device is as figure 1 As shown, it includes a base part, a longitudinal movement part, a lateral movement part, a rotating part and a top platform part.
[0018] The base part includes a base body 2, casters 10, a support height adjustment seat 11, an end support 12 and an end support shaft 13. The base body 2 is an H-shaped structural welding structure, which can realize small size and large span bearing; 4 casters 10 are installed under the base body 2 for the movement of the entire equipment; the end support 12 is installed on the base through the end support shaft 13 On the main body 2, the end support 12 can rotate 90 degrees around the end support shaft 13; the four corners of the end support 12 are respectively equipped with support height adjustment seats 11 for supporting and height ad...
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The invention discloses butt joint and regulation equipment for solar wings of a moonlet. The equipment comprises a base part, a longitudinal movement part, a transverse movement part, a rotation part and a top layer platform part. Through the movements of the longitudinal movement part, the transverse movement part and the rotation part, the moonlet fixed in the top layer platform part can move in different directions at different angles, thereby realizing the regulation of six degrees of freedom of the body of the moonlet when the solar wings of the moonlet is butt-jointed, solving the problem of regulation for the body of the moonlet when the solar wings of the moonlet are butt-jointed, improving safety coefficient, improving regulation precision, greatly lowering the working intensity of personnel, and improving working efficiency.
Description
Technical field [0001] The invention belongs to the technical field of satellite tests, and particularly relates to a small satellite solar wing docking test adjustment device. Background technique [0002] During the docking test between the small satellite and the solar wing, it is necessary to ensure the relative position of the interface between the small satellite and the solar wing. The specific process of the docking between the star and the solar wing is as follows: first use the simulation wall to adjust the position of the solar wing, and then dock the satellite star mounted on the carriage with the solar wing. When the satellite is docked with the solar wing, it is difficult to ensure that the parking position of the carriage is just the position required for the docking test. At this time, the only way to ensure the docking position is to adjust the position of the satellite, that is, to adjust the position of the support car equipped with the satellite. [0003] The ...
Claims
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IPC IPC(8): B64G1/64
Inventor 刘江张名毅王凤彬梁小峰薛长利周传君肖连辉
Owner AEROSPACE DONGFANGHONG SATELLITE