Airborne Monitoring System AMOS
Airborne data server (AMOS) by SPEEL PRAHA Ltd. company is designed to:
- gather, process, and record information about airborne systems of the light combat aircraft L159 with the goal to offer the pilot information about the instant aircraft situation including warnings when the limit values are reached
- watch and monitor the load on the airframe in the long term
- record data for air crash evaluation
- watch and monitor the health state of the pilot
The AMOS system consists of the following two parts:
- cockpit units:
- FDAU159CAF unit for reading data
- FSP159CAF functional signal panel
- CMU159CAF crash data recorder
- ground units that are designed to maintain AMOS system and ensures:
Communication interface:
- RS-232C
- RS-422
Standards:
- MIL-STD-1553B
- MIL-STD-704E
- MIL-STD-810E
- MIL-STD-461D
- MIL-STD-462D
- EUROCAE ED-55
- TSO-C124
Technical parameters:
Size:
| CMU159CAF: | 124 x 231,5 x 121,5 mm |
| FDAU159CAF: | 236 x 267 x 201 mm |
| FSP159CAF: | 146 x32 x 72 mm |
Weight:
| CMU159CAF: | < 5 kg |
| FDAU159CAF: | < 10 kg |
| FSP159CAF: | < 0,20 kg |
Memory size:
| CMU159CAF: | 16 MB |
| FDAU159CAF: | 4 MB |
Power supply:
| CMU159CAF: | 18 to 32 Vss |
| FDAU159CAF: | 18 to 32 Vss |
| FSP159CAF: | 8,5 to 25 Vss |
Energy input:
| CMU159CAF: | maximal 7 W |
| FDAU159CAF: | maximal 30 W |
| FSP159CAF: | maximal 9 W |
MTBF:
| CMU159CAF: | 10 000 flight hours |
| FDAU159CAF: | 3 000 flight hours |
| FSP159CAF: | 20 000 flight hours |
Service temperature:
-54°C to +60°C
Total technical life of AMOS system:
25 years (8 000 flight hours)
Service guarantee:
see technical conditions of the units
- copying the flight parameters from FDAU159CAF and CMU159CAF memories using either the ground supporting units (GSU) by SPEEL PRAHA Ltd. company or portable memory units (PMU)
- detailed data processing, evaluation, and browsing
- long-term monitoring using various program modules included in PANDA system