A sequence of ground and flight simulation experiments was conducted to investigate helicopter instrument-flight-rules airworthiness criteria. The first six of these experiments and major results are summarized. Five of the experiments were conducted on large-amplitude motion base simulators. The NASA-Army V/STOLAND UH-1H variable-stability helicopter was used in the flight experiment. Artificial stability and control augmentation, longitudinal and lateral control, and in pitch and roll attitude augmentation were investigated. Previously announced in STAR as N82-23219
A summary of NASA/FAA experiments concerning helicopter IFR airworthiness criteria
1983-07-01
Sonstige
Keine Angabe
Englisch
Helicopter Airworthiness Symposium : Proceedings
TIBKAT | 1984
|Airworthiness Certification Criteria
NTIS | 2004