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Stabilität
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keywords:(Stabilität)
Free-flight and free-oscillation techniques for wind-tunnel dynamic-stability testing
Simulation Evaluation of Pilot Inputs for Real Time Modeling During Commercial Flight Operations
Position Corrections for Airspeed and Flow Angle Measurements on Fixed-Wing Aircraft
Flight Test Results on the Stability and Control of the F-15 Quiet Spike(TradeMark) Aircraft
Design of Low Complexity Model Reference Adaptive Controllers
In-Trail Procedure Air Traffic Control Procedures Validation Simulation Study
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
Implementation of an Adaptive Controller System from Concept to Flight Test
Stability and Control Analysis of the F-15B Quiet SpikeTM Aircraft
Aeroservoelastic Stability Analysis of the X-43A Stack
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
Crew Procedures for Continuous Descent Arrivals Using Conventional Guidance
Tailored Excitation for Frequency Response Measurement Applied to the X-43A Flight Vehicle
Flight Dynamics Analysis Branch End of Fiscal Year 2005 Report
Control Laws for a Wind Tunnel Free-Flight Study of a Blended-Wing-Body Aircraft
Bias Momentum Sizing for Hovering Dual-Spin Platforms
Development of Handling Qualities Criteria for Rotorcraft with Externally Slung Loads
Vertical Motion Simulator Experiment on Stall Recovery Guidance
A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design
Flight Test Implementation of a Second Generation Intelligent Flight Control System
The case for inherent stability of helicopters
Stability of nonlinear vehicle systems
Manual Manipulation of Engine Throttles for Emergency Flight Control
Autonomous Guidance of Agile Small-scale Rotorcraft
Air Traffic Management Technology Demostration-1 (ATD-1) Avionics Phase 2 Flight Test and Results
Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System
Modeling and Analysis of Large Amplitude Flight Maneuvers
Flight Test Results for the F-16XL With a Digital Flight Control System
Enabling CSPA Operations Through Pilot Involvement in Longitudinal Approach Spacing
Towards a Formal Semantics of Flight Plans and Trajectories
A Fuzzy Technique for Performing Lateral-Axis Formation Flight Navigation Using Wingtip Vortices
Vertical Navigation Control Laws and Logic for the Next Generation Air Transportation System
Reconstruction of the Apollo 11 Moon Landing Final Descent Trajectory
Real-Time Stability and Control Derivative Extraction From F-15 Flight Data
UAV Flight Control Using Distributed Actuation and Sensing
On Wings of the Minimum Induced Drag: Spanload Implications for Aircraft and Birds
Design Requirements for Unmanned Rotorcraft Used in Low-Risk Concepts of Operation