Structure analysis and work results of the mathematical simulation stands for the rocket and space technology control systems development

Author:

Miljuchenko S. G.,Kashirtsev K. B.,Nesterenko A. N.,Nichushkina T. N.,Ilek O. S.,Sgonnikov A. S.,Kaznacheev S. A.

Publisher

AIP Publishing

Reference22 articles.

1. Stevens, B. L., Lewis, F. L., & Johnson, E. N. (2015). Aircraft control and simulation: dynamics, controls design, and autonomous systems. John Wiley & Sons.

2. Milyuchenko S.G., Kashirtsev K.B., Dmitriev V.S., Nesterenko A.N., Bolshakov M. V. (2014). Unificirovannyj stend matematicheskogo modelirovaniya RKT [Unified stand for mathematical modeling of rocket-space technology] // Raketnye kompleksy i raketno-kosmicheskie sistemy – proektirovanie, eksperimental’naya otrabotka, lyotnye ispytaniya, ekspluataciya: Trudy sekcii 22 imeni akademika V.N. CHelomeya XXXVIII Akademicheskih chtenij po kosmonavtike. Posvyashchayutsya 100-letiyu so dnya rozhdeniya V.N. Chelomeya [Rocket complexes and rocket-space systems - design, experimental development, flight tests, operation: Proceedings of section 22 named after academician V.N. Chelomey]. Reutov, JSC Military-industrial corporation NPO Mashinostroenia, 362–364.

3. The computer program 2014611715 Russian Federation. The software package “Yadro” SADI.00373-01 [text]. Miluchenko S.G. [and etc.]; Applicant and rightholder JSC Military-industrial corporation NPO Mashinostroenia. - N 2013618136; declare 09/12/2013; publ. 03/20/2014.

4. Синтез законов ковариационного управления космическим аппаратом

5. Kosyanchuk V.V., Selvesyuk N.I., Chuyanov G.A. (2013). Problems of development of technologies for the design of aircraft avionics for military purposes. Armament and Economics, 13, 42–48.

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