DOI 10.17586/0021-3454-2017-60-3-229-233
UDC 004.031.43
ARCHITECTURE OF SOFTWARE AND HARDWARE COMPLEXES OF ON-BOARD EQUIPMENT
M. V. Lomonosov MSU, Department of Computer Systems Automation;
Read the full article
Abstract. The main features of the avionics systems with federated and integrated modular architecture are considered. The causes, which can lead to increased hardware costs when running functional programs in real-time in complexes with integrated modular architecture are analyzed by the example of a location system.
Keywords: real-time systems, embedded systems, integrated modular avionics, program, virtual channe
References:
References:
- ARINC 651-1, Design Guidance for Integrated Modular Avionics, 1997.
- Arinc Specification 653. Airlines Electronic Engineering Committee, http://www.arinc.com.
- Godunov A.N., Soldatov V.A. Programming and Computer Software, 2014, no. 5, pp. 69–76. (in Russ.)
- Kostenko V.A. Automation and Remote Control, 1994, no. 12, pp. 151–162. (in Russ.)
- Kostenko V.A. Programming and Computer Software, 1997, no. 2, pp. 67–75.(in Russ.)
- Shukalov A.V., Paramonov P.P., Kniga E.V., Zharinov I.O. Informatsionno-upravliaiushchie sistemy (Information and Control Systems), 2014, no. 5, pp. 64–71. (in Russ.)
- Balashov V.V., Kapitonova A.P., Kostenko V.A., Smelyanskiy R.L., Yushchenko N.V. Programming and Computer Software, 1999, no. 5, pp.52–61.(in Russ.)
