Optimization of calculation algorithm for models developed with a method based on three-stage decomposition
Authors: Pavlov D.V., Petrov D.S.
Published in issue: #8(56)/2016
DOI: 10.18698/2308-6033-2016-8-1522
Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering
The article considers the development of service systems computer models on board the spacecraft. We describe existing approaches to computer modeling, their features for such technical systems; propose a new approach which, firstly, allows us to consider the various physical interactions that occur in the system, secondly, to structure the model and, thirdly, to present it as a uniform element set. The study suggests the algorithm that makes it possible to build a software representation of the state vector and propose settlement functions of the system under study, based on a formal description of its model, made in accordance with the described approach to modeling. On the base of the algorithm we developed a computer program. The study estimates the computer program speed and the possibility of using an original approach to modeling service systems on board the spacecraft in order to inform spacecraft flight control and describes the measures to further performance improving.
References
[1] Solovev V.A., Lysenko L.N., Lyubinskiy V.E. Upravlenie kosmicheskimi poletami [Mission control]. Moscow, BMSTU Publ., 2009, 902 p.
[2] Kravets V.G. Avtomatizirovannye sistemy upravleniya kosmicheskimi poletami [Automated mission control system]. Moscow, Mashinostroenie Publ., 1995.
[3] Mikrin E.A. Bortovye kompleksy upravleniya kosmicheskikh apparatov [On board spacecraft control systems]. Moscow, BMSTU Publ., 2014, 245 p.
[4] Trudonoshin V.A. Modelirovanie sistem s sosredotochennymi parametrami [Modeling of systems with lumped parameters]. 2008. Available at: http://bigor.bmstu.ru/?cnt/?doc=BaseCourse (accessed June 5, 2016).
[5] Aksenov A.A., Dyadkin A.A., Moskalev I.V. Kosmicheskaya tekhnika i tekhnologii - Space technics and technologies, 2015, no. 2, pp. 39-50.
[6] Alabova N.P., Bryukhanov N A., Dyadkin A.A. et al. Kosmicheskaya tekhnika i tekhnologii - Space technics and technologies, 2014, no. 3, pp. 14-21.
[7] Antonov F.K., Makarovskaya A.V., Papchenko V.V., Shaenko A.Yu. Vestnik MGTU im. N.E. Baumana. Seriya Mashinostroenie - Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering, 2015, no. 1, pp. 49-55.
[8] Paynter H. Analysis and design of engineering systems. Cambridge, MIT Press Publ., 1961, 303 p.
[9] Mukheijee A., Samantaray A.K. Bond graph in modeling, simulation and fault identification. New Delhi, India, I.K. International Pvt. Ltd. Publ., 2006, 512 p.
[10] Petrov D.S. VestnikMoskovskogo Aviatsionnogo Instituta - Herald of Moscow Aviation Institute, 2014, vol. 21, no. 1, pp. 43-57.
[11] Pavlov D.V., Petrov D.S. Vestnik Moskovskogo Aviatsionnogo Instituta - Herald of Moscow Aviation Institute, 2015, vol. 22, no. 2, pp. 42-54.
[12] Rotten B. van de, Lunel S. A limited memory Broyden method to solve highdimensional systems of nonlinear equations. The Netherlands, Mathematisch Instituut, Universiteit Leiden Publ., 2003, 236 p.