EFFECTS OF TYROSCOPIC CROSS COUPLING BETWEEN PITCH AND YAW ON THE HANDLING QUALITIES OF VTOL AIRCRAFT
Abstract
A visual flight investigation indicates the extent to which cross coupling affects handling qualities as a function of engine angular momentum, angular velocity about the yaw axis, and longitudinal control power. A theoretical examination, supplemented by simulator data, indicates the extent to which increased longitudinal damping improves the coupling controllability.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1961
- Accession Number
- AD0265914
Entities
People
- John F. Jr. Garren
Organizations
- National Aeronautics and Space Administration