Flowfield Analysis of Vortex Interactions During Large Sharp-Edged Gusts
Postflight Assessment of Mars 2020 Entry, Descent, and Landing Simulation
The Effect of Installation Power Losses on the Overall Performance of a Helicopter
Ice Protection System Design for the Next Generation Civil Tiltrotor Engine Intake
Snow Effects on the NGCTR Nacelle for Relevant Certification Conditions
Air Bleed Objective for Rotorcraft Turbine Engines
Fuzzy Adaptive Nonsingular Terminal Sliding Mode Control of a Miniature Helicopter
Experimental Analysis of Advanced Control and Estimation Systems for Autonomous Ship Landing
Optimal Planetary Surface Exploration with Heterogeneous Agents
Pilots’ Perspectives on Urban Air Mobility Safety Challenges and Potential Solutions
Simultaneous swept anhedral helicopter blade tip shape and control-system design
Method to Calculate Behind Start of Takeoff Roll Noise Level Adjustments
Design Concepts to Meet EASA SC-VTOL-01 Single Failure Criteria
Flight Dynamics and Control of an Unmanned Helicopter with Underslung Double Pendulum
Comparison of Autonomous Flight Control Performance Between Partial- and Full-Authority Helicopters
Real-Time Prediction of Probabilistic Crack Growth with a Helicopter Component Digital Twin
Rapid Method for Computing Reachable Landing Distances in Helicopter Autorotative Descent
New Algorithm and Experiments for Helicopter Active Control of Structural Response
Cable-Suspended Cooperative Transportation Control with Multi-unmanned Helicopters
Designation of Direction of Rotation of Helicopter Rotors
One-Parameter Optimal Flux Reconstruction Schemes for Adaptive Mesh Refinement
Comment on “Analysis of Helicopter Handling Quality in Turbulence with Recursive von Kármán Mode”
XGBoost Gradient-Boosted Tree Predictions Using Limited Data for Coaxial Rotor Helicopters
Active Vibration Control of Helicopter Fuselage with Large Dynamic Modeling Errors
Three-Dimensional Dynamics of Towed Underslung Systems Using Geometrically Exact Beam Theory
Aerodynamic Interaction Effects Between Propellers in Typical eVTOL Vehicle Configurations
Airfoil Method for Rotary Wing Analysis Using Modified Lift and Drag Equations
Considerations for Medically-Fit Rotary-Wing Aircrew in Future Operations: A Summary Report