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Stabilität
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keywords:(Stabilität)
Modeling of Large-Amplitude High-Angle-of-Attack Maneuvers
Model order reduction applied to a hot-bench simulation of an aeroelastic wind-tunnel model
Modified Cascading Generalized Inverse Control Allocation
Modified Cascading Generalized Inverse Control Allocation
Multi-Objective Optimal Control of High Aspect Ratio Wing Wind Tunnel Model
NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
Navier-Stokes prediction of large-amplitude delta-wing roll oscillations characterizing wing rock
Neural network application to aircraft control system design
New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity
New literal approximations for the longitudinal dynamic characteristics of flexible flight vehicles
Numerical Simulation of Rolling-Airframes Using a Multi-Level Cartesian Method
Off-Nominal Event Analysis in Autonomous Flights Based on Explainable Artificial Intelligence
Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression
Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression
Overview of Active Flow Control Actuator Development at NASA Langley Research Center
Plans and Example Results for the 2nd AIAA Aeroelastic Prediction Workshop
Predictor-Based Model Reference Adaptive Control