93-3890 Spacecraft Intercept Guidance Using Zero Effort Miss Steering
2011-6374 Maturity Enhancements for Aircraft Simulation for Traffic Operations Research
Aeroelastic Vehicle Multivariable Control Synthesis with Analytical Robustness Evaluation
AIAA-2002-4750 Optimal Blending Filter Parameters and Sensor Placement for Flight Control
AIAA-2002-4784 New Methodology for Single Parameter Robust Spacecraft Control Analysis and Synthesis
AIAA-2004-4755 Life Extension Control for a Highly Maneuverable Vehicle
AIAA-2006-1649 Underload Injection Effect on Optimal Overload Values for Crack Growth Retardation
AIAA-2006-1650 Mean Stress Effect on Optimal Overload for Crack Mitigation in Aircraft Panels
AIAA-2006-6338 Descent Management Strategies for Future Small Aircraft Transportation Systems
Aircraft Acceleration Prediction With Flight Data Validation Due To Atmospheric Disturbances
Aircraft Spin Phenomenon Analysis Using Nonlinearity Index Theory
Aircraft Stall Phenomenon Analysis Using Nonlinearity Index Theory
Aircraft Volterra Parameter-Varying Modeling Approach
Airspace Encounter Models for Estimating Collision Risk
Analytical Expressions for Linear Quadratic Aeroelastic Flight Control Eigenvalues
ANALYTICAL NONLINEAR ANALYSIS METHODOLOGY FOR REDUCED AIRCRAFT DYNAMICAL SYSTEMS
Analytical Relationships for Linear Quadratic Aeroelastic Flight Control Eigenvalues
Analytical Solution of Uniaxial Flight Systems Using Volterra Kernels in Frequency Domain