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Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements

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Abstract

The article deals with the task to estimate microaccelerations caused by natural oscillations of big elastic elements after impulse firing of an orientation system engine. Offered estimation is useful for development of space-system engineering intended for realization of gravity-sensitive processes. It can be applied for taking a decision about appropriateness of one or another process on the board of spacecraft.

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  1. Samara State Aerospace University of the name of academician S.P. Korolev, Samara, Russian Federation

    A. V. Sedelnikov

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  1. A. V. Sedelnikov
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Sedelnikov, A.V. Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements. Microgravity Sci. Technol. 28, 491–498 (2016). https://doi.org/10.1007/s12217-016-9507-8

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  • DOI: https://doi.org/10.1007/s12217-016-9507-8

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