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ON THE METHOD OF SYNTHESIS OF OPTIMAL CONTROL OF SPACECRAFT REORIENTATION DURING SENSING HARDWARE REDIRECTION
- Authors: Morozova M.1
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Affiliations:
- Institute for the Control of Complex Systems of RAS
- Issue: Vol 19, No 9.2 (2013)
- Pages: 208-214
- Section: Articles
- URL: https://journals.ssau.ru/est/article/view/4727
- DOI: https://doi.org/10.18287/2541-7525-2013-19-9.2-208-214
- ID: 4727
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Abstract
The problem of optimal control of spacecraft reorientation during remote earth sensing hardware redirection is considered. Computational algorithm for the approximate solution of the problem is developed. Efficiency of this algorithm is confirmed by the results of the performed modeling.
About the authors
M.V. Morozova
Institute for the Control of Complex Systems of RAS
Author for correspondence.
Email: morenov.sv@ssau.ru
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