FAHRZEUGDIFFERENZIAL MIT RINGFÖRMIGEN VERSCHLUSSRING ZUM LÖSBAREN KOPPELN DES DIFFERENZIALGEHÄUSES
Model-Free Adaptive State Feedback Control for a Class of Nonlinear Systems
Composite panel with wireless, self-powered or remotely powered sensing assembly
UNMANNED LOGISTICS VEHICLE, TRANSACTION SYSTEM AND METHOD
Analysis of Rotor Noise During Maneuvering Flight Based on CLORNS Solver
Analysis of Rotor Noise During Maneuvering Flight Based on CLORNS Solver
INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX
Control method and system of unmanned logistics vehicles
CONTROL METHOD AND SYSTEM OF UNMANNED LOGISTICS VEHICLES
SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045
MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM
HEIGHT-VELOCITY CHARACTERISTICS COMPARISONS OF SINGLE-ROTOR AND COAXIAL HELICOPTERS
HEIGHT-VELOCITY CHARACTERISTICS COMPARISONS OF SINGLE-ROTOR AND COAXIAL HELICOPTERS
FLIGHT PERFORMANCE AND TRAJECTORY PREDICTION OF THE COAXIAL HELICOPTER IN AUTOROTATION
ANALYTICAL MODELLING OF A HOVERABLE X-SHAPE FLAPPING WING AIRCRAFT CONSIDERING WING-TAIL INTERACTION
ANALYSIS OF AERODYNAMIC COUPLING EFFECT IN CLOSE FORMATION FOR FLAPPING WINGS
A Deep Learning-Based Approach to Resource Allocation in UAV-aided Wireless Powered MEC Networks
BESCHICHTETE KOHLENSTOFFFASERVERSTÄRKTE POLYMERE VERBUNDWERKSTOFFE FÜR DEN KORROSIONSSCHUTZ
COATED CARBON FIBER REINFORCED POLYMERIC COMPOSITES FOR CORROSION PROTECTION
HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS
Dynamic output feedback sliding mode control for uncertain linear systems
Locomotion Adaptation in Heavy Payload Transportation Tasks with the Quadruped Robot CENTAURO
MODELING AND CONTROL OF A HOVERABLE FLAPPING WING AIRCRAFT CONSIDERING FLAPPING WING INDUCED FLOW
PRELIMINARY DESIGN OF SEVERAL NEW KINDS OF MARTIAN AIRCRAFTS
PRELIMINARY DESIGN OF SEVERAL NEW KINDS OF MARTIAN AIRCRAFTS
PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL
PROGRESS OF BLENDED-WING-BODY AIRCRAFT DEVELOPMENT AT NORTHWESTERN POLYTECKNICAL UNIVERSITY