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Stabilität
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keywords:(Stabilität)
Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis
Stratospheric Test Methodology for Characterizing Free-Flight Dynamics of Entry Vehicles
NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
UAS Well Clear Recovery Against Non-Cooperative Intruders Using Vertical Maneuvers
Aerodynamic Design of the Hybrid Wing Body Propulsion-Airframe Integration
Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies
GOES-R Active Vibration Damping Controller Design, Implementation, and On-Orbit Performance
Development of Mission Adaptive Digital Composite Aerostructure Technologies (MADCAT)
ADEPT Sounding Rocket One (SR-1)Flight Experiment Overview
Integrated Insulation System for Automotive Cryogenic Storage Tanks
150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model
Capsulation Satellite or CapSat: A Low-Cost, Reliable, Rapid-Response Spacecraft Platform
Aerodynamic Design of Integrated Propulsion-Airframe Configuration of the Hybrid Wing-Body Aircraft
Evaluating the Autonomous Flying Qualities of a Simulated Variable Stability Aircraft
Investigating the Transonic Flutter Boundary of the Benchmark Supercritical Wing
Status of Computational Aerodynamic Modeling Tools for Aircraft Loss-of-Control
Investigation of Desiccants and CO2 Sorbents for Advanced Exploration Systems 2015-2016
Update on Risk Reduction Activities for a Liquid Advanced Booster for NASA's Space Launch System
Nonlinear Unsteady Aerodynamic Modeling Using Wind Tunnel and Computational Data
Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Active Structural Control for Aircraft Efficiency with the X-56A Aircraft
Iraq Stability: Foreign Military Sales in a New War Environment
Use of Higher Fidelity Slosh Models to Reduce Conservatism in Launch Vehicle Flight Control Designs
Earth Entry Vehicle Design for Sample Return Missions Using M-SAPE
Application and Evaluation of Control Modes for Risk-Based Engine Performance Enhancements
Need for the United States Army to Possess a Landing Craft with Maneuver Capabilities
Fixed-Wing Aircraft Simulation Tool for Improving the efficiency of DoD Acquisition
Evaluation and Validation of Organic Materials for Advanced Stirling Convertors (ASCs): Overview
Recent Flight Control System Analyses in Support of Space Launch System
Tip-over Prevention Through Heuristic Reactive Behaviors for Unmanned Ground Vehicles
Piloted Simulation of a Model-Predictive Automated Recovery System
Space Launch System Implementation of Adaptive Augmenting Control
Liquefied Bleed for Stability and Efficiency of High Speed Inlets
Liquefied Bleed for Stability and Efficiency of High Speed Inlets
Designing Liquid Rocket Engine Injectors for Performance, Stability, and Cost