Co-design Optimization of a Novel Multi-identity Drone Helicopter (MICOPTER). [PDF]
J Intell Robot Syst, 2022 Abedini A, Bataleblu AA, Roshanian J.
europepmc +1 more source
Design, Analysis, and Testing of a Hybrid VTOL Tilt-Rotor UAV for Increased Endurance. [PDF]
Sensors (Basel), 2021 Panigrahi S, Krishna YSS, Thondiyath A.
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, 2010 Due to the recent increase in development and use of co-axial rotor system at the scale of small UAVs a greater understanding of the performance variables that affect the co-axial propulsion system at low Reynolds number operation has become increasingly
Brazinskas, Mantas +4 more
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Robust tracking control for a quadrotor subjected to disturbances using new hyperplane-based fast Terminal Sliding Mode. [PDF]
PLoS One, 2023 Labbadi M +4 more
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Large-Pitch Hovering Control of Tilt Tri-Rotor UAVs Using Symmetric Control Formulation
IEEE Transactions on Industrial ElectronicsLarge-pitch hovering can substantially extend the maneuvering envelope of tilt tri-rotor unmanned aerial vehicles (TTR UAVs), but it also introduces strong orientation-dependent coupling that limits the applicability of conventional multirotor control formulations.
Xutao Qu, Zhihao Cai, Yingxun Wang
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Design a model and mathematical approach for vectored trust controlled tri rotor aerial platform
, 2018 It is a challenging factor to address the more or less of vectored trust-controlled platforms for Stability. There are unnecessary parts in any UAV plat form and must be identified and apply removal of such parts or substitute with aerodynamically more ...
Madanayaka HM
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Development of Non Expensive Technologies for Precise Maneuvering of Completely Autonomous Unmanned Aerial Vehicles. [PDF]
Sensors (Basel), 2021 Bigazzi L +3 more
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A decentralized hybrid computing consumer authentication framework for a reliable drone delivery as a service. [PDF]
PLoS One, 2021 Hannan A +6 more
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Advances on intelligent algorithms for scientific computing: an overview. [PDF]
Front Neurorobot, 2023 Hua C, Cao X, Liao B, Li S.
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Helicopter tail rotor thrust and main rotor wake coupling in crosswind flight [PDF]
, 2010 The tail rotor of a helicopter with a single main rotor configuration can experience a significant reduction in thrust when the aircraft operates in crosswind flight. Brown’s vorticity transport model has been used to simulate a main rotor and tail rotor
Fletcher, Timothy M., Brown, Richard
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