With the advancement of electric vehicles towards intelligence and integration, four-wheel independent drive (FWID) vehicles, characterized by high controllability and structural flexibility, have gained widespread attention.
Zhiqi Guo +5 more
doaj +1 more source
Musculoskeletal wing-actuation model of hummingbirds predicts diverse effects of primary flight muscles in hovering flight. [PDF]
Agrawal S +5 more
europepmc +1 more source
Conceptual design, evaluation and research identification for Remote Augmented Propulsive Lift Systems (RALS) with ejectors for VTOL aircraft [PDF]
Ejector concepts for use with a remote augmented lift system (RALS) exhaust nozzle were studied. A number of concepts were considered and three were selected as having the greatest promise of providing the desired aircraft and exhaust gas cooling and ...
Konarski, M. +2 more
core +1 more source
Hummingbirds use wing inertial effects to improve manoeuvrability. [PDF]
Haque MN, Cheng B, Tobalske BW, Luo H.
europepmc +1 more source
Reconfigurable Control Design of Steering and Torque Vectoring Based on Reachability Set Analysis [PDF]
Castro +10 more
core +1 more source
Preliminary study of VTO thrust requirements for a V/STOL aircraft with lift plus lift/cruise propulsion [PDF]
A preliminary assessment was made of the VTO thrust requirements for a supersonic (Type B) aircraft with a Lift plus Lift/Cruise propulsion system. A baseline aircraft with a takeoff gross weight (TOGW) of 13 608 kg (30,000 lb) was assumed.
Allen, J. L., Turney, G. E.
core +1 more source
Research on control effectiveness of fluidic thrust vectoring. [PDF]
Xue F, Yunsong G, Wang Y, Qin H.
europepmc +1 more source
On the passive limited slip differential for high performance vehicle applications [PDF]
The paper is aimed at a comprehensive revision of the working principles and limitations of the mechanical limited slip differential, the traditional, passive device used to improve traction capabilities and to extend the performance envelope of high ...
Chindamo, Daniel +2 more
core
Study of Modeling and Optimal Take-Off Scheme for a Novel Tilt-Rotor UAV. [PDF]
Yu Z, Zhang J, Wang X.
europepmc +1 more source

