Results 71 to 80 of about 1,986 (195)

Flybbit: Design and Control of a Novel Rabbit-like Flying Robot

open access: yesDrones
In this paper, we present the design and control of a novel aerial vehicle inspired by the biomechanics of a rabbit named “Flybbit”. Flybbit consists of two main components, namely a movable “Ears” part and a rigid “Body” part, forming a composite flying
Chenyang Sun   +5 more
doaj   +1 more source

A Resilient Approach to a Test Rig Setup in the Qualification of a Tilt Rotor Carbon Fiber-Reinforced Polymer (CFRP) Wing

open access: yesAerospace
The evolution of aircraft wing development has seen significant progress since the early days of aviation, with static testing emerging as a crucial aspect for ensuring safety and reliability.
Pasquale Vitale   +6 more
doaj   +1 more source

Analysis of the influence of transition state control strategy on structural load of quad-tiltrotor

open access: yesHangkong gongcheng jinzhan
There are complex structural load changes in the rotor during the tilt-transition of quad-tiltrotor aircraft,which can directly affect the life of the rotor.
HE Yongtao   +3 more
doaj   +1 more source

Longitudinal Integrated Attitude Control Law Design and Robustness Analysis of Tiltrotor Aircraft

open access: yesNanjing Hangkong Hangtian Daxue Xuebao
Since the tiltrotor aircraft needs to switch configurations among helicopter mode, transition mode, and fixed-wing mode within its flight envelope, and its dynamic characteristics vary significantly under different configurations, it is necessary to ...
CHEN Guojun, LIU Yi, ZHANG Wei
doaj   +1 more source

Long-short term memory networks for modeling track geometry in laser metal deposition. [PDF]

open access: yesFront Artif Intell, 2023
Perani M   +4 more
europepmc   +1 more source

Co-design Optimization of a Novel Multi-identity Drone Helicopter (MICOPTER). [PDF]

open access: yesJ Intell Robot Syst, 2022
Abedini A, Bataleblu AA, Roshanian J.
europepmc   +1 more source

Virtual Full Scale Static Test of a Civil Tilt Rotor Composite Wing in Non-Linear Regime

open access: yesAerospace
This study addresses the crucial role of post-buckling behavior analysis in the structural design of composite aeronautical structures. Traditional engineering practices tend to result in oversized composite components, increasing structural weight. EASA
Antonio Chiariello   +6 more
doaj   +1 more source

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