Satellite-borne cold atom imprisoning-type acceleration measurement method
A technology of acceleration measurement and cold atom, which is applied in the direction of using inertial force for acceleration measurement, measurement device, measurement of gravitational field, etc. It can solve the problem of different force characteristics of cold atoms, limit the engineering feasibility of cold atom ejection method, and improve the accuracy of acceleration measurement. Difficulty and other problems, to achieve the effect of simple operation, promotion of application, and improvement of measurement accuracy
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[0044] The present invention will be described in detail below with reference to specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that, for those skilled in the art, several modifications and improvements can be made without departing from the concept of the present invention. These all belong to the protection scope of the present invention.
[0045] A spaceborne cold atom trapped acceleration measurement method, comprising the following steps:
[0046] Step 1: Load the alkali metal atoms into the three-dimensional magneto-optical trap, install the three-dimensional magneto-optical trap at the center of mass of the satellite, and connect it to the main body of the satellite through a bracket.
[0047] Considering that there is only one valence electron in the outer layer of the alkali metal atom, and the energy level structure is...
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