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Standsicherheit
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A Robust Uniform Control Approach for VTOL Aircraft
A Robust Uniform Control Approach for VTOL Aircraft
Reference Command Optimization for the Transition Flight Mode of a Lift plus Cruise Vehicle
NASA Armstrong Flight Research Center Dynamics and Controls (530)
System Identification of Flexible Aircraft: Lessons Learned from the X-56A Phase 1 Flight Tests
Control of Flexible Spacecraft with Structural Feedback
Free-Flight CFD Simulations and Dynamic StabilityAnalysis of the Orion Crew Module
Preliminary Steps in Developing Rapid Aero Modeling Technology
Multipropeller Whirl Flutter Stability Study using Component Mode Synthesis Element