Disclosed is a
satellite-borne cold atom imprisoning-type acceleration measurement method.
Alkali metal atoms are filled in a three-dimensional magnetic-optical trap, the three-dimensional magnetic-optical trap emits a beam of
alkali metal atoms to the space, the
alkali metal atoms are stopped by an oncoming
laser beam and are introduced to central points of the
laser beam and a
magnetic field, the central point of the
laser beam, the central point of the
magnetic field and the
mass center of a
satellite coincide, and the intensity of the laser beam and the
magnetic field is controlled to enable the position of a cold atom to be kept in the position of the
mass center of the
satellite. In the operation process of the satellite, when the action force on the satellite and the action force on the cold atom are different, the cold atom deviates from the
mass center of the satellite, so that the
control force of the laser and the magnetic field is changed, and corresponding
control force of the laser and the magnetic field are applied to enable the cold atom to be back to position of the
mass center. The variation of the
control force of the laser and the magnetic field in the operation process of the satellite in the third step is measured, and acceleration of the cold atom relative to the
mass center of the satellite, namely the acceleration of non-
inertia force on the satellite is calculated. The satellite-borne cold atom imprisoning-type acceleration measurement method has the advantages of being high in measurement accuracy, high in
engineering feasibility and simple in operation.