A series of flight tests were conducted on the PC 9/A aircraft, A23- 045 at the Royal Australian Air Force's Aircraft Research and Development Unit System identification techniques were applied to the data obtained from these flight tests to determine the stability and control derivatives of the aircraft. The longitudinal results for the aircraft in cruise configuration are presented in this report and comparisons are made with empirical and ground based estimates.
Correlation Between Flight-Determined Longitudinal Derivatives and Ground-based Data for the Pilatus PC 9/A Training Aircraft in Cruise Configuration
2000
45 pages
Report
Keine Angabe
Englisch