ROBUST OPTIMAL INPUT DESIGN FOR FLIGHT VEHICLE SYSTEM IDENTIFICATION
Optimal Input Design for Flight Vehicle System Identification in Frequency Domain
On the Flight Test Campaign of a Coaxial Helicopter for the Development of an Unmanned Aerial System
HELICOPTER PARAMETER ESTIMATION BASED ON A NONLINEAR PHYSICS-BASED MODEL
Flight-Test Plan Design and Evaluation in a Closed-Loop Framework for a General Aviation Aircraft
Excitation Monitoring for Online Parameter Estimation
Development and Validation of an Inflow Model for a Coaxial Teetering Rotor System