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DEVELOPMENT OF THE MATHEMATICAL MODEL, ALGORITHM AND SOFTWARE FOR SELECTION OF THE SPACECRAFT PROTECTION AGAINST IMPACT OF THE METEORITES AND SPAСE DEBRIS
https://doi.org/10.15518/isjaee.2016.21-22.045-054
Abstract
The paper deals with the sources of high speed bodies and particles of the natural and artificial origin which are dangerous for the spacecraft operation. The paper presents the parameters of certain groups of the meteoric particles and the sources space debris. The following ways allow the spacecrafts to avoid collision with space debris: change of spacecraft orbit, and optimal protection of the spacecraft surface. An actual problem of creation of the spacecraft protection for spacecraft operating on the near Earth orbit for a long time includes development of the algorithms and software for the optimization of spacecraft screen protection and reduce mass. Development of the algorithms and software for the spacecraft multiunit protection solves the problem of optimization of spacecraft surface screen multi-unit protection for basic models as cube and cylinder (in the algorithmic languages of Fortran and BUILDER-4) by the method of dynamic programming with Pareto sets. Moreover, we developed the visualization programs of the optimization results and the utilities that provide interface of the calculating programs and databases in Windows environment. The programs include plotting, providing the calculation clearness.
About the Authors
A. G. Galeev
Science and Testing Center of the Rocket-Space Industry
Russian Federation
D.Sc. (engineering), Professor, Laureate of USSR Council of Ministers in the field of science and technology, member of the RACTs, Chief Researcher of the PCF “SIC RSI”, Professor of “Management of Operation of RSS”
Russian Federation
D.Sc. (engineering), Professor, Laureate of USSR Council of Ministers in the field of science and technology, member of the RACTs, Chief Researcher of the PCF “SIC RSI”, Professor of “Management of Operation of RSS”
V. N. Kadantsev
Moscow Technological University
Russian Federation
D.Sc. (physics and mathematics), Professor, Member of the New York Academy of Sciences, Russian Ecological Academy, the Head of the Applied Synenergetics Department
Russian Federation
D.Sc. (physics and mathematics), Professor, Member of the New York Academy of Sciences, Russian Ecological Academy, the Head of the Applied Synenergetics Department
Y. V. Zakharov
Moscow Technological University
Russian Federation
Russian Federation
D. N. Mikhaylov
S.A. Lavochkin Scientific and Production Association
Russian Federation
D.Sc. (engineering), Professor of the Applied Synergetics Department
Russian Federation
D.Sc. (engineering), Professor of the Applied Synergetics Department
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Review
For citations:
Galeev A.G., Kadantsev V.N., Zakharov Y.V., Mikhaylov D.N. DEVELOPMENT OF THE MATHEMATICAL MODEL, ALGORITHM AND SOFTWARE FOR SELECTION OF THE SPACECRAFT PROTECTION AGAINST IMPACT OF THE METEORITES AND SPAСE DEBRIS. Alternative Energy and Ecology (ISJAEE). 2016;(21-22):45-54. (In Russ.) https://doi.org/10.15518/isjaee.2016.21-22.045-054
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