Abstract
The design and realization of avionics integrated simulation system about mission computer system was introduced. The functions, composition and the methods of the hardware and software were discussed on emphasis. The system adopted the bus topological structure of a certain aircraft, connecting the various subsystems so as to display, process, control and transmit the data integratedly and share resource. This system could be used in the avionics simulation system for experiment and its feasibility and correctness were validated.
| Original language | English |
|---|---|
| Pages (from-to) | 2904-2906+2920 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 21 |
| Issue number | 10 |
| State | Published - 20 May 2009 |
Keywords
- Avionics integrated simulation
- Bus topological structure
- Digital simulation
- Mission computer system