Impact of Varied Power Setting on Thrust of Multi-Rotor VTOL sUAS in Ground Effect (AIAA 2017-0226)
A De-Spin and Wings-Leveling Controller for a 40 mm Hybrid Projectile
Potentials of Phlegmatization in Diesel Hybrid Electric Vehicles
Towards Model-Driven Development of Hard Real-Time Systems: Integrating ASCET and aiT/StackAnalyzer