Aircraft Motion Sensitivity to Cross and Cross-Coupling Damping Derivatives
Abstract
An investigation was conducted to provide some insight into the importance of dynamic cross and cross-coupling derivatives in motion simulation studies of fighter aircraft in the maneuvering flight regime. The aircraft motion sensitivity to the various derivatives is ascertained in level and turning flight utilizing a 5 deg of freedom linearized stability program. The results are presented in a root locus format.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1976
- Accession Number
- ADA032654
Entities
People
- R. W. Butler
Organizations
- Arnold Engineering Development Complex