Different procedures for the analysis of flight test data in order to obtain stability characteristics are presented. Methods discussed include: time vectors, forced oscillations, analog matching, and regression analysis. Notwithstanding the considerable difficulties in data measurement, the task of evaluating aircraft characteristics from flight data is indispensable for setting up reliable mathematical models to describe the dynamic behavior of the aircraft.
Determination of Aircraft Characteristics from Flight Tests
1974
260 pages
Report
Keine Angabe
Englisch