A system of compensating rotary microacceleration by a magnetic method

Abstract


The paper deals with a system that uses a magnetic method of compensating microaccelerations and does not require changing the design of a space vehicle (SV). The results of modelling the motion relative to the centre of mass for different types of SV are given.


About the authors

N. D. Syomkin

Samara State Aerospace University

Author for correspondence.
Email: sadohina@ssau.ru

Russian Federation

V. L. Balakin

Samara State Aerospace University

Email: sadohina@ssau.ru

Russian Federation

K. Ye. Voronov

Samara State Aerospace University

Email: sadohina@ssau.ru

Russian Federation

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