Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
  • Русский
  • Английский
Article

Rationale for engineering design characteristics of spacecraft groups based on a probabilistic approach

Published: 16.09.2016

Authors: Zolotov A.A., Nurullaev E.D.

Published in issue: #10(58)/2016

DOI: 10.18698/2308-6033-2016-10-1539

Category: Power, Metallurgic and Chemical Engineering | Chapter: Hydraulic Machines and Hydropneumatic units

The study tested the optimization problem of design and engineering characteristics of spacecraft groups, its solution requiring the probabilistic approach. We evaluated the indicator of the target program performance effectiveness with minimized costs. Moreover, we developed the methods and software to optimize the probability of failure and the redundancy multipleness of on-board systems, as well as the resource, the number of substitutions and the number of redundant spacecraft. While using optimization techniques, we also applied Lagrange methods, as well as search and random search methods. The efficiency of the proposed approach is illustrated by definite examples. The findings of the research can serve as a guide for engineering and technical personnel of enterprises in the development of highly reliable products of rocket and space technology.


References
[1] Novozhilov G.V., Neymark M.S., Tsesarskiy L.G. Bezopasnostpoleta samoleta. Kontseptsiya i tekhnologiya [Aircraft flight safety. The concept and technology]. Moscow, Mashinostroenie Publ., 2003, 144 p.
[2] Anfimov N.A., Budilov Yu.G. Kosmonavtika i raketostroenie - Cosmonautics and Rocket Engineering, 1996, no. 7, pp. 58-65.
[3] Zolotov A.A., Odelevskiy V.K., Rodchenko V.V., Chernikov A.I. Prikladnye metody i algoritmy obespecheniya nadezhnosti i bezopasnosti tekhnicheskikh sistem na etape ikh razrabotki i ekspluatatsii [Applied methods and algorithms to ensure the reliability and safety of technical systems at the stage of their development and operation]. Moscow, MAI Publ., 2013, 352 p.
[4] Zolotov A.A., Nurullaev E.D. Polet - Flight, 2015, no. 3, pp. 57-64.