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Standsicherheit
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A Robust Uniform Control Approach for VTOL Aircraft
Reference Command Optimization for the Transition Flight Mode of a Lift plus Cruise Vehicle
System Identification of Flexible Aircraft: Lessons Learned from the X-56A Phase 1 Flight Tests
Control of Flexible Spacecraft with Structural Feedback
Free-Flight CFD Simulations and Dynamic StabilityAnalysis of the Orion Crew Module
Preliminary Steps in Developing Rapid Aero Modeling Technology
An L1 Adaptive Control Augmentation for a Lift Plus-Cruise Vehicle
Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements
Control Concepts for Simplified Vehicle Operations of a Quadrotor eVTOL Vehicle
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Development of the Mod II X-57 Piloted Simulator and Flying Qualities Predictions
Flutter Analysis of the Transonic Truss-Braced Wing Aircraft Using Transonic Correction
Dynamic Aeroelastic Flight Dynamic Modeling of Mach 0.745 Transonic Truss-Braced Wing
The Impact of Structural Vibration on Flying Qualities of a Supersonic Transport
Loss of Control Detection for Commercial Transports Using Conditional Variational Autoencoders
Mode-Based Sensing and Actuation Techniques for Multi-Objective Flexible Aircraft Control
Aircraft System Identification from Multisine Inputs and Frequency Responses
Time-varying Weights in Multi-Objective Optimal Control for Flexible Wing Aircraft
Multi-Objective Flight Control for Ride Quality Improvement for Flexible Aircraft
Trajectory Generation for Noise-Constrained Autonomous Flight Operations
Piloted Simulator Evaluation Results of Flight Physics Based Stall Recovery Guidance
Learn-To-Fly (L2F): Real-Time Modeling, Learning Control, and Guidance for Autonomous Flight
Link!: Potential Field Guidance Algorithm for In-Flight Linking of Multi-Rotor Aircraft
Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies
Estimation, Navigation and Control of Multi-Rotor Drones in an Urban Wind Field
Real-Time Global Nonlinear Aerodynamic Modeling for Learn-To-Fly
Aeroelastic Modeling of X-56A Stiff-Wing Configuration Flight Test Data
Air STAR Beyond Visual Range UAS Description and Preliminary Test Results
Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis
High-Fidelity Flight Dynamic Analysis of Transonic Truss-Braced Wing
Toward n-Ship Computation of Trajectories for Shared Airspace
Dynamic Modeling from Flight Data with Unknown Time Skews
Establishing a Disruptive New Capability for NASA to Fly UAV's into Hazardous Conditions
Design and Analysis of Morpheus Lander Flight Control System
A Generic Nonlinear Aerodynamic Model for Aircraft
Autonomous Guidance Algorithms for NASA Learn-to-Fly Technology Development
Descent and Landing Triggers for the Orion Multi-Purpose Crew Vehicle Exploration Flight Test-1
Performance Enhancement of a Vertical Tail Model with Sweeping Jet Actuators