Flight Dynamics Analytically-Derived Mathematical Model of Tiltrotor Aircraft: The development of an approachable tilt-rotor flight mechanics model, with clearly defined limitations, suitable for performance and piloted flight simulation

Comparative Flight Performance Evaluation of the Flying-V and a Reference Aircraft

Flight Mechanics and Performance of Direct Lift Control: Applying Control Allocation Methods to a Staggered Box-Wing Aircraft Configuration

A Control Allocation approach to induce the center of pressure position and shape the aircraft transient response

A trim problem formulation for maximum control authority using the Attainable Moment Set geometry

Handling Qualities of a Flying V Configuration

On the Necessary Degrees of Freedom for Helicopter and Wind Turbine Low-Frequency Mode Modeling

Optimum cruise performance of subsonic transport aircraft