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NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
Candidate Performance Metrics for Generalized Control for Autonomous Flight
Summary of the First AIAA Stability and Control Prediction Workshop
Flight Test of L1 Adaptive Controller on the NASA AirSTAR Flight Test Vehicle
F-15 Intelligent Flight Control System and Aeronautics Research at NASA Dryden
L(sub 1) Adaptive Control Design for NASA AirSTAR Flight Test Vehicle
Integrated Resilient Aircraft Control Project Full Scale Flight Validation
AERONAUTICAL LAB. EXAMINATION OF RECENT LATERAL-STABILITY-DERIVATIVE DATA
Implementation of an Adaptive Controller System from Concept to Flight Test
Pilot Evaluation of Adaptive Control in Motion-Based Flight Simulator
Effect of steady rolling on longitudinal and directional stability
Stability and Control Derivative Estimation for the Bell-Shaped Lift Distribution
Adaptive Flight Control for Aircraft Safety Enhancements
Full Scale Advanced Systems Testbed (FAST): Capabilities and Recent Flight Research
Intelligent Contingency Management for Urban Air Mobility
Variable-Structure Control of a Model Glider Airplane
Simulation Based Evaluation of Integrated Adaptive Control and Flight Planning Technologies
Recent System Identification Research at NASA Langley Research Center
Intelligent Contingency Management for Urban Air Mobility
Flight Test Results on the Stability and Control of the F-15B Quiet Spike Aircraft
Stability and Control Analysis of the F-15B Quiet Spike Aircraft
Piloted Simulation Study of Rudder Pedal Force/Feel Characteristics
Rapid Aero Modeling for Urban Air Mobility Aircraft in Computational Experiments
Verification and Validation Challenges for Adaptive Flight Control of Complex Autonomous Systems
Stability Characteristics of the Apollo Command Module
The NASA Langley Challenge on Optimization Under Uncertainty
Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression
Channel-wing System for Thrust Deflection and Force/Moment Generation
Equation of Motion for a Generic Multibody Tilt-rotor Aircraft
Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression
System Identification of the X-56A from Flight Test Data --- Status Update
Framework for ensuring runtime stability of control loops in multi-agent networked environments
Adaptive Optimization for System Performance: Parameterized Differential Dynamic Programming
Classifying Aircraft using Velocity Data with Support Vector Machines and Likelihood Ratio Tests