Adaptive Aircraft Control in the Presence of Unstructured Dynamic Uncertainties
Adaptive Flight Control Under Actuation and Sensor Failures and Slow-Engine Dynamics
Addendum 3 Lateral Control and Stability Surfaces
Adverse-Yaw Control During Roll for a Class of Optimal Lift Distributions
Aerodynamics analysis of the main rotor influence on the static stability of the gyroplane
Aeronautic Conceptual Design Optimization Method Based on High-Order Singular Value Decomposition
Aerostructural Design Optimization Using a Multifidelity Quasi-Newton Method
Aircraft stability and control model using wavelet transforms
Aircraft System Identification from Multisine Inputs and Frequency Responses
Air Vehicle Enviroment in C++: A Computational Design Environment for Conceptual Innovations
Alternative Trim Analysis Formulations for Vehicles with Redundant Multi-Axis Control Surfaces
A Method to Improve the Aircraft Aerodynamic Characteristics at High Angles of Attack and in Spin
An elastic element of the forced oscillation apparatus for dynamic wind tunnel measurements