Method of the Autonomous Indirect Identification of the Conversion Factor of Pendulum Compensating Accelerometer Under the Conditions for the Orbital Flight of Automatic Spacecraft
Keywords:
Pendulum Compensating Accelerometer, Conversion Factor, Graphical Analysis, Oscillatory System, Aperiodic System, Transient Response, DerivativeAbstract
Is examined the method of the autonomous indirect identification of the conversion factor of pendulum compensating accelerometer, which makes it possible with the high accuracy to determine the coefficient under the conditions for orbital flight indicated by the built-in firmware means of this gauge and to, thus, decrease an error in the determination of increase in the apparent in the velocity with the accomplishment of maneuver by automatic spacecraftReferences
Published
2015-06-15
How to Cite
Mironov, V., Fominov, I., & Maletin, A. (2015). Method of the Autonomous Indirect Identification of the Conversion Factor of Pendulum Compensating Accelerometer Under the Conditions for the Orbital Flight of Automatic Spacecraft. SPIIRAS Proceedings, 3(40), 93-109. https://doi.org/10.15622/sp.40.7
Section
Articles
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