Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation

In this paper, we consider the main aspects of a problem in formation and control of a required microacceleration level as the most important characteristic of the space laboratory intended for realizing the gravitational and sensitive technological processes. The estimation model and methodology to...

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Published in:Russian aeronautics 2014-04, Vol.57 (2), p.111-117
Main Authors: Belousov, A. I., Sedel’nikov, A. V.
Format: Article
Language:English
Subjects:
Automotive Engineering
Construction
Engineering
Estimates
Flight Vehicle Design
Formations
Mathematical models
Methodology
Space laboratories
Spacecraft
Spacecraft design
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description In this paper, we consider the main aspects of a problem in formation and control of a required microacceleration level as the most important characteristic of the space laboratory intended for realizing the gravitational and sensitive technological processes. The estimation model and methodology to control and estimate the microaccelerations are presented that are necessary for the well-founded choice of the spacecraft parameters and carrying out their flight and space tests, when the new special-purpose space laboratories are designed and constructed.
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subjects Automotive Engineering
Construction
Engineering
Estimates
Flight Vehicle Design
Formations
Mathematical models
Methodology
Space laboratories
Spacecraft
Spacecraft design
title Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation
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