Global Aircraft Dynamics Using Piecewise Volterra Kernels
Aircraft Spin Phenomenon Analysis Using Nonlinearity Index Theory
Aircraft Stall Phenomenon Analysis Using Nonlinearity Index Theory
The Application of Quaternion Algebra to Gyroscopic Motion, Navigation, and Guidance AIAA Paper
AIAA-2006-1650 Mean Stress Effect on Optimal Overload for Crack Mitigation in Aircraft Panels
ANALYTICAL NONLINEAR ANALYSIS METHODOLOGY FOR REDUCED AIRCRAFT DYNAMICAL SYSTEMS
Global Stability and Control Derivative Modeling Using Design of Experiments
Relative Motion Guidance, Navigation and Control for Autonomous Spacecraft Rendezvous (AAS 11-212)
Dynamics at Cusp Points on the Repeating Orbits (AAS 11-247)
Relative Motion Modeling and Control in a Perturbed Orbit (AAS 11-211)
Stability Derivative Modeling Based on Aircraft Flight Modes Using Design of Experiments
Development of a High Accuracy MEMS Angular Measurement System for Hypersonic Wind Tunnel Facilities
Transition Boundaries at the Collinear Libration Points
Keeping a Spacecraft on a Vertical Circular Orbit around an Earth-Moon Lagrange Point (AAS 09-344)
Optimal Overload Ratio Age Dependency in Fatigue Crack Growth