AIAA-2002-4667 Improving Control Allocation Accuracy for Nonlinear Aircraft Dynamics
AIAA-2004-4871 Stability Domain Estimation for Dynamic Inversion Embedded SDRE Flight Controller
AIAA-2004-5017 Reconfigurable Control Design for the X-40A with In-Flight Simulation Results
AIAA-2004-5168 Methods for Compensating for Control Allocator and Actuator Interactions
Altitude Control of a Single Degree of Freedom Flapping Wing Micro Air Vehicle
A Method for Including Control Effector Interactions in the Control Allocation Problem AIAA Paper
Combined Reference Governor and Anti-Windup Design for Constrained Hypersonic Vehicles Models
Computation of Inertial Forces and Torques Associated with Flapping Wings
Control Allocation of Reaction Control Jets and Aerodynamic Surfaces for Entry Vehicles AIAA Paper
Dynamics and Control of a Minimally Actuated Biomimetic Vehicle: Part I - Aerodynamic Model
Dynamics and Control of a Minimally Actuated Biomimetic Vehicle: Part II-Control
Flapping Wing Micro-Air-Vehicle 4-DOF Controller Applied to a 6-DOF Model
Flapping Wing Micro-Air-Vehicle Control, Employing Triangular Wave Strokes and Cycle-Averaging
LPV Control Design for Over-Actuated Hypersonic Vehicles Models
Neural Dynamic Trajectory Design for Reentry Vehicles AIAA Paper