Disk wing as a solution of some “eternal” problems of main rotor
Design, Modeling, and Testing of Hybrid-Electric Fixed-Wing VTOL Aircraft Propulsion System
Influence on Vertical Landing Stability of Multirotor UAVs with Adaptive Landing Gears
Conceptual Design and System Level Analysis of Tilt-Duct eVTOL Aircraft
Data-Driven Urban Air Mobility Flight Energy Consumption Prediction and Risk Assessment
Parametric Identification of a Return Space Vehicle during Vertical Landing
Analysis of trimmable conditions for a civil aircraft with active high-lift system
Effect of an active high-lift system failure during landing approaches
Stabilization of the vertical take-off of a rigid flying wing for an airborne wind energy system
A starting system for measuring low airspeeds of a single-rotor helicopter
Wheels, Brakes, and Landing Gear
Control Scheme for Automatic Takeoff and Landing of Small Electric Helicopter
Research on Obstacle-Crossing Characteristic for Air Cushioned Transport Aircraft
The New Paradigm of Safe and Sustainable Transportation: Urban Air Mobility
Nonlinear Modeling of Fixed-Wing Mode for a Ducted-Fan Tiltrotor UAV by DATCOM
Flight Dynamics Modeling and Simulation of Propeller Deflected Slipstream VTOL Aircraft
A starting system of warning the critical conditions for a single-rotor helicopter
Urban Airspace Route Planning for Advanced Air Mobility Operations