Helicopter Guidance and Control Systems.
Abstract
;Contents: Military helicopter requirements; Low speed control to landing on instruments in helicopters; An optimum military helicopter navigation system; Automatic flight control system for light helicopters; An integrated low altitude flight control system for helicopters; Subsystems; Advanced development; Test results and operational experience.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1971
- Accession Number
- AD0731670
Entities
Organizations
- AGARD