| Design / Development |
- System Engineering
- Simultaneous Design Engineering
- Processor For Development And Management Of Radiated Inorganic Gage Software
- Avionics System /System And Component Design
- Component Interlocking Design
|
- Obtain Voice And Flight Data / Process / Demonstrate
- Flight Regime, Exceedance , Usage
- Integrity Monitoring Algorithm
- Rotor Track And Balance Algorithm
- Noise Filtering
- Data Convergence
|
Requires No System Redevelopment |
| HW |
- Storage Design
- Visualization Device Design
- Device Driver, API Development
- MIL Standard Base Design
- MIL-STD-810, MIL-STD-461, MIL-STD-704,
DO-160, DO-254
|
- Flash Memory Design
- USB/Ethernet Interface
- NVIS Compatible Design
- CPU/FPGA/DSP Base Design
- VME, PCIe Bus Design
- Communications Interface Design
- 1553B, ARINC-429, CAN, RS-422등
|
-
 Development Processor
Board PCB (Example)
-
 Development of Acceleration/Tachometer Sensor Channel and HW for HUMS(Example)
|
| SW |
- Real Time OS, ARINC-653 Based OS Mounting
- DO-178C Level C
- DAPA Weapon System Software Development Management Processor
|
- Static/Dynamic Testing
- Database Link
- Stand Alone / Web-based Linked Design
|
|
| Sub-System |
- Processor Board
- Voice, Signal Processing Board
- Analog, Sensor Data Processing Board
- Power Supply Board
- Backplane
|
- OFP Development
- Firmware Development
- Sensor Interlocking
- Sensor/ Processor Integral Module
- Data Fusion
|
|
| Development Technology for Testing Equipment |
- Development of Test Equipment Based on Setting Information
- Systematic Signal Simulations
- Monitoring Transmission Data
|
- Set-up Information-Based Signal Simulation
- Analog/Transfer/Digital Data, Etc.
- Sensor Data
- About HW Channels
|
- System Integration Test Equipment
- ATE Equipment, Etc.
|
