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Stabilität
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COOREFLEX-Turbo : Vorhaben-Nr. 1.3.1b : "Robustes Aero Design" : Abschlussbericht
Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis
Free-flight and free-oscillation techniques for wind-tunnel dynamic-stability testing
SinSee - Beurteilung der Schiffssicherheit in schwerem Seegang : Schlussbericht
Simulation Evaluation of Pilot Inputs for Real Time Modeling During Commercial Flight Operations
Active Structural Control for Aircraft Efficiency with the X-56A Aircraft
Position Corrections for Airspeed and Flow Angle Measurements on Fixed-Wing Aircraft
In-Trail Procedure Air Traffic Control Procedures Validation Simulation Study
Flight Test Results on the Stability and Control of the F-15 Quiet Spike(TradeMark) Aircraft
Design of Low Complexity Model Reference Adaptive Controllers
Design and Control of an Experimental Tilt-Wing Aircraft
An Adaptive Control Technology for Safety of a GTM-like Aircraft
Full-Scale Prop-Rotor Stability Tests on the XV3 at High Advance Ratios
NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
Stability and Control of Maneuvering High-Performance Aircraft
Implementation of an Adaptive Controller System from Concept to Flight Test
Stability and Control Analysis of the F-15B Quiet SpikeTM Aircraft
Crew Procedures for Continuous Descent Arrivals Using Conventional Guidance
Aeroservoelastic Stability Analysis of the X-43A Stack
Tailored Excitation for Frequency Response Measurement Applied to the X-43A Flight Vehicle
Guidance and Control of an Autonomous Soaring UAV
Guidance and Control of an Autonomous Soaring UAV
Autonomous Airborne Refueling Demonstration, Phase I Flight-Test Results
Vertical Motion Simulator Experiment on Stall Recovery Guidance
Stability and Control Derivatives of the T-37B Airplane
Flight Dynamics Analysis Branch End of Fiscal Year 2005 Report
The Influence of Short Springs on Longitudinal Static Stability
Bias Momentum Sizing for Hovering Dual-Spin Platforms
Control Laws for a Wind Tunnel Free-Flight Study of a Blended-Wing-Body Aircraft
The case for inherent stability of helicopters
Development of Handling Qualities Criteria for Rotorcraft with Externally Slung Loads
Flight Test Implementation of a Second Generation Intelligent Flight Control System
A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design
Stability of nonlinear vehicle systems
Low-Subsonic Flight and Force Investigation of a Supersonic Transport Model with a Double-delta Wing
Flight Test Results for the F-16XL With a Digital Flight Control System
Determination of Aircraft Characteristics from Flight Tests
Effects of Structural Flexibility on Spacecraft Control Systems