The Integrated Flight Control Computer (IFCC) is the central control computer for the RPFA. IFCC consists of flight control computer, Air Data Computer, Aircraft Encoder Decoder unit. The Single Channel Tester is the automatic test equipment to test the IFCC. SCT shall be used to perform the hardware ATP of IFCC.
SCT is a portable test equipment to check the electrical functionalities of IFCC by simulating various signals and pressure in standalone conditions. System able to simulate, acquire, monitor, and validate the functionalities of different signals.
Specifications
- Portable unit for standalone operation
- CPCI based Architecture
- Powerful SBC with RTOS (Linux) — Compatible with AETS software architecture for ease of development
- Shall be used for Hardware ATP clearance of IFCC
- 19" Rack based Tester with Advanced 6U size Compact Tester
- Operates on 230VAC
-
Tester have following I/O (Click to Expand)
- Discrete Input output - 192
- Analog Input Output - 144
- LVDT, RVDT, DCM, Excitation Sets - 20
- Frequency Outputs - 4
- Primary Actuator Interface with Inductive Loads - 10 (1 spare)
- Secondary Actuator Interface with Inductive Loads - 2 (1 spare)
- SPIL - 4
- CCDL - 8
- MIL1553B - 3
- ASYNC RS422 - 24
- SYNC RS422 - 6
- Differential IO - 32
- Inbuilt LRU Power Supply to power IFCC
- Self test facility at connector level
- Calibration Facility
- All Outputs are Monitored at Connector end of Tester
- Provision to feed real sensor signals and measurement
- Failure Simulation for required signals
- Status Indication at Front Panel
- IO interfaces at Rear panel
Environmental Specifications
- Operating Temperature: 0 to +55°C
- Storage Temperature: -40 to +85°C
- Humidity: 95% Relative (Non-condensing) @ 40°C
Cost
Rs. 2, 25, 00, 000/- Plus applicable Taxes