Computing Systems Configuration for Highly Integrated Guidance and Control Systems
Abstract
Contents: Computing System Configuration for Fighter Aircraft Flight Control Systems; A Highly Reliable Computer for Airborne Applications; Testing Embedded Software; Advanced Avionics Architecture - Pave Pillar; Data and Signal Processing Architectures for Future Avionics; Fiber Optic Buses and Networks for Advanced Avionics Architectures; High Speed Parallel Processing Networks for Advanced Architectures.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1988
- Accession Number
- ADA199308
Entities
Organizations
- AGARD