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Journal Information-measuring and Control Systems №3 for 2020 г.
Article in number:
Synthesis technique software components aviation multifunctional simulators
UDC: 004.94
Authors:

L.E. Mistrov – Dr.Sc.(Eng.), Associate Professor, Professor, 

MESC «Zhukovsky–Gagarin Air Force Academy» (Voronezh)

E-mail: mistrov_le@mail.ru

E.M. Shepovalov – Head of Flight Simulator, 

MESC «Zhukovsky–Gagarin Air Force Academy» (Voronezh)

E-mail: shepovaloff2011@yandex.ru

Abstract:

Existing models of flight simulators are designed to solve a limited set of training problems and have a number of significant drawbacks, the main of which is the limited ability to solve the problems of adaptation and optimization of software algorithms for aviation multifunction flight simulators (AMT software) when new training problems arise, as well as the complexity and labor intensity in practical use.

The synthesis methodology for software components (PC) software is based on the formation of sets of elementary operations (EO) and PC, corresponding to the real functional, logical, executive (physical) and information processes in the simulation of training tasks AMT. It allows you to formalize the information process of building a PC, to develop algorithms for the adaptive use of AMT to solve newly arising educational problems, and to optimize the software formation process according to selected criteria. It is based on the justification of the primary table for constructing a PC as a function of the totality of determining EE and their parameters.

The solution to the problem of building a PC is based on optimizing the number of EOs involved, allowing to implement the principle of adapting software operation algorithms for various ways of using AMT. Its solution is based on the application of the branch and bound method, which ensures the reduction and ordering of the process of enumerating PC variants based on the initial splitting of the set of EO (PC) into groups determined by the number of units in rows (EO) and in columns (PC) and minimizing rows (columns) inside each group when forming a PC.

Pages: 28-35
References
  1. Mistrov L.E., Shepovalov E.M. Osnovy prinyatiya reshenii po razrabotke (modernizatsii) aviatsionnykh mnogofunktsionalnykh trenazherov. Uspekhi sovremennoi radioelektroniki. 2019. № 6. S. 66−76. DOI: 10.18127/j20700784-201906-08. (In Russian).
  2. Mistrov L.E., Mishin A.V., Shepovalov E.M. Metod strukturno-parametricheskogo sinteza programmnogo obespecheniya aviatsionnykh mnogofunktsionalnykh trenazherov. Uspekhi sovremennoi radioelektroniki. 2020 (v pechati). (In Russian).
  3. Mistrov L.E., Shepovalov E.M.  Metod formirovaniya variantov elementarnykh tekhnologicheskikh operatsii realizatsii uchebnykh zadach aviatsionnym mnogofunktsionalnym trenazherom. Naukoemkie tekhnologii. 2020 (v pechati). (In Russian).
  4. Mistrov L.E., Shepovalov E.M. Metod resheniya zadachi sinteza informatsionno-obuchayushchikh sistem upravleniya radioelektronnymi obieektami. Internet-zhurnal «Informatsionno-ekonomicheskie aspekty standartizatsii i tekhnicheskogo regulirovaniya». 2018. № 3(43). (In Russian).
  5. Mistrov L.E., Belotserkovskii I.O., Plotnikov S.N. Osnovy vydeleniya tipovykh uslovii konfliktnogo vzaimodeistviya strukturno slozhnykh sistem. Naukoemkie tekhnologii. 2018. T. 19. № 11. S. 4−7. DOI: 10.18127/j19998465-201811-01. (In Russian).
Date of receipt: 6 февраля 2020 г.