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Stabilität
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keywords:(Stabilität)
Active Control of Separation From the Flap of a Supercritical Airfoil
Mitigating Motion Base Safety Issues: The NASA LaRC CMF Implementation
Wake Vortex Tracking Using a 35 GHz Pulsed Doppler Radar
A Fast-Time Simulation Environment for Airborne Merging and Spacing Research
Post-Stall Aerodynamic Modeling and Gain-Scheduled Control Design
Flight Test of the F/A-18 Active Aeroelastic Wing Airplane
Free-to-Roll Investigation of Uncommanded Lateral Motions for an Aircraft with Vented Strakes
Dynamics Modeling and Simulation of Large Transport Airplanes in Upset Conditions
Design of a Multi-mode Flight Deck Decision Support System for Airborne Conflict Management
Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System
Attitude Control for an Aero-Vehicle Using Vector Thrusting and Variable Speed Control Moment Gyros
Free-to-Roll Investigation of Uncommanded Lateral Motions for an Aircraft With Vented Strakes
Advanced Video Guidance Sensor and Next Generation Autonomous Docking Sensors
Pathway Design Effects on Synthetic Vision Head-Up Displays
Overview of Intelligent Systems and Operations Development
18-Degree-of-Freedom Controller Design for the ST7 Disturbance Reduction System
Control Reallocation Strategies for Damage Adaptation in Transport Class Aircraft
Dynamic Stall Measurements and Computations for a VR-12 Airfoil with a Variable Droop Leading Edge
Characterization of Passive Dynamic Stability of a Microwave Sail
Cost Estimation and Control for Flight Systems
Overview of Active Flow Control Actuator Development at NASA Langley Research Center
An Adaptive Critic Approach to Reference Model Adaptation
Optimal Aircraft Control Upset Recovery With and Without Component Failures
Numerical Simulation of Rolling-Airframes Using a Multi-Level Cartesian Method
Living with a Star Space Environment Testbed
Visualizing Decision-making Behaviours in Agent-based Autonomous Spacecraft
A Roadmap for Aircraft Engine Life Extending Control
Cartesian-Grid Simulations of a Canard-Controlled Missile with a Free-Spinning Tail
Intelligent Control Approaches for Aircraft Applications
Stability and Control Properties of an Aeroelastic Fixed Wing Micro Aerial Vehicle
Flight Test Experience With an Electromechanical Actuator on the F-18 Systems Research Aircraft
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
Flight Control System Development for the BURRO Autonomous UAV
Use of Individual Flight Corridors to Avoid Vortex Wakes
Flight Control Using Distributed Shape-Change Effector Arrays
Flight Control Role in RLV Configuration Development
Multidisciplinary Techniques and Novel Aircraft Control Systems
Multidisciplinary Techniques and Novel Aircraft Control Systems
Flying Quality Analysis of a JAS 39 Gripen Ministick Controller in an F/A-18 Aircraft
Utilizing Flight Data to Update Aeroelastic Stability Estimates
Closed-Loop Hybrid Flight Management Systems
Full-Scale Wind Tunnel Studies of F/A-18 Tail Buffet
Laminar Flow Control Leading Edge Systems in Simulated Airline Service