Flight test results of Observer / Kalman Filter Identification of the Pegasus unmanned vehicle


Flight testing is the preferred means of obtaining accurate, locally linear, dynamic models of nonlinear aircraft dynamics. In this paper, decoupled longitudinal and lateral/directional linear dynamic models of an unmanned air vehicle are identified using the Observer/Kalman Filter Identification method. This method is a time-domain technique that… (More)

16 Figures and Tables


  • Presentations referencing similar topics