Airborne safety critical system development we can help you
- Formulate detailed system & sub-system level requirements from high level user requirements
- Validate System Level Requirements
- Prepare the development documents required for airborne systems in accordance with ARP-4754A / ED-79A
- Reliability Analysis as per Mil-HDBK-217
- Carry out complete System Safety Analysis of perceived and existing products as per ARP-4761A/ED-135
- Carry out basic design work for any airborne product abiding by Model Based Design approach as per RTCA DO-331 / EUROCAE ED-218
- Provide C and VHDL Code Generation Certifiable as per RTCA DO 178C/ED-12C & RTCA DO-254/ED80
- Detailed Verification and Validation Plans
Aircraft EMC Test Analysis
- Develop test Plans as per SAE ARP 5583A/ ED-91; AC 20-158A /AMC 20-158 & RTCA DO-160G/ED-14G
- Finalize Test Plans for Mil-Std-461G & Mil-Std-464D
- Computation of Low Level Coupling Tests for HIRF Compliance
- Aircraft Antenna Placement Analysis
- Predicting Platform and Systems EMC compliance through simulations
- Predicting EMC compliance of electronic products as per commercial EMC standards
Coverage and Integrity Analysis of Communication Navigation and Surveillance Avionics
System Development as per RTCA DO-331 / EUROCAE ED-218
Model Based System Engineering (MBSE) for complete system development
Design of RF Front Ends for Avionics and Radar Systems
Systems Modeling and Simulation
Avionics Obsolescence Management