2022
DOI: 10.1038/s41598-022-05367-9
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Modeling the disturbing effect on the aist small spacecraft based on the measurements data

Abstract: The paper considers the issues of reconstruction of the power disturbing effect on the prototype of the small spacecraft "Aist". The measurements data of the components of the induction vector of the Earth's magnetic field by means of two three-component magnetometers were used for the reconstruction. The obtained results can be used to assess microaccelerations in the internal environment of small spacecraft, as well as to study their uncontrolled rotational motion.

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Cited by 13 publications
(19 citation statements)
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“…The mass of this device is 39 kg, including 11 kg of equipment for scientific research. Pilot model of the Aist small spacecraft and used coordinate systems: OX0Y0Z0 is the bench coordinate system in which the components of the small spacecraft inertia tensor were determined (point О is the geometric center of a small spacecraft); CXYZ is the main body axis coordinate system with the origin at the center of mass (point C) of a small spacecraft; xcyczc is the structural coordinate system of magnetometer № 2 (this coordinate system is left) (cited of [20]).…”
Section: Mathematical Model For a Small Spacecraft Rotational Motionmentioning
confidence: 99%
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“…The mass of this device is 39 kg, including 11 kg of equipment for scientific research. Pilot model of the Aist small spacecraft and used coordinate systems: OX0Y0Z0 is the bench coordinate system in which the components of the small spacecraft inertia tensor were determined (point О is the geometric center of a small spacecraft); CXYZ is the main body axis coordinate system with the origin at the center of mass (point C) of a small spacecraft; xcyczc is the structural coordinate system of magnetometer № 2 (this coordinate system is left) (cited of [20]).…”
Section: Mathematical Model For a Small Spacecraft Rotational Motionmentioning
confidence: 99%
“…Let us estimate the significance for each of the disturbing influences included in equation ( 1). During ground tests of Aist small spacecraft pilot model, the axial and centrifugal moments of inertia in the axes of the test bench were experimentally established (OX0Y0Z0) [10,20]…”
Section: Mathematical Model For a Small Spacecraft Rotational Motionmentioning
confidence: 99%
See 3 more Smart Citations