System Safety: MIL-STD-882, ARP4761, ARP4754, JSSG-2006, MIL-STD-1472G; Software/Hardware Safety: DO-178C Level A/B, MIL-STD-498, and DO-254; AC 20-138A, AC 25-11; Airworthiness Certification Criteria - MIL-HDBK-516B; Environmental /EMI/Power - MIL-STD-810, DO-160D, MIL-STD-461, MIL-STD-704; NASA System Safety - Avionics and Software Safety.
Program Verification and Validation represent the plan, processes, best practices for certification. V&V planning reflects the structure of the program by defining the verification and validation activities performed against system level integration and associated subsystems. V&V planning defines the approach for requirements verification and validation.
Private cloud-based infrastructure, server operating system, with a 99% uptime-availability service level agreement (SLA). Designed to support complete web application lifecycle: building, testing, deploying, managing, and updating. The cloud-based hosting platform and network infrastructure will secure, robust solution delivery platform.
Software development for avionics boxes, emulators, and FPGAs. Functional allocation, Software Design Verification Objectives (DVOs), Unit Testing, and DVO Success Criteria.
Embedded software (hardware) for board level FPGAs, modeling, testing, and documentation.