Application of Parameter Estimation to Highly Unstable Aircraft
The Identification of Linear Ship Steering Dynamics Using Maximum Likelihood Parameter Estimation
Active Aeroelastic Wing Aerodynamic Model Development and Validation for a Modified F/A-18A
Effects of Wing Modification on an Aircraft's Aerodynamic Parameters as Determined from Flight Data
Parameter Estimation Techniques and Application in Aircraft Flight Testing
Active Aeroelastic Wing Aerodynamic Model Development and Validation for a Modified F/A-18A Airplane
Development of a Simple, Self-Contained Flight Test Data Acquisition System
Localization of a Submerged Tow Vehicle (Lost)
Stability and Control Derivative Estimates Obtained from Flight Data for the Beech 99 Aircraft
Estimation of the Aircraft State in Non-Steady Flight