Airbus A320 and Electrically Signaled Actuators
Optimization of Landing Control for Shipborne Unmanned Aerial Vehicles Based on Total Energy Control
Dynamic Modeling of Main Landing Gear of a High-Altitude Long Endurance UAV
Direct Lift Control of Carrier-Based Aircraft Based on Thrust Vector
Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft
Airport Capacity and Configuration