Zobrazeno 1 - 10
of 68
pro vyhledávání: '"Hoang Vu Phan"'
Autor:
Mohammad Askari, Michele Benciolini, Hoang-Vu Phan, William Stewart, Auke J. Ijspeert, Dario Floreano
Publikováno v:
Communications Engineering, Vol 3, Iss 1, Pp 1-13 (2024)
Abstract Perching with winged Unmanned Aerial Vehicles has often been solved by means of complex control or intricate appendages. Here, we present a method that relies on passive wing morphing for crash-landing on trees and other types of vertical po
Externí odkaz:
https://doaj.org/article/04a1ec42aa8a4aafa957765d95e36780
Publikováno v:
Royal Society Open Science, Vol 3, Iss 12 (2016)
This study used numerical and experimental approaches to investigate the role played by the clap-and-fling mechanism in enhancing force generation in hovering insect-like two-winged flapping-wing micro air vehicle (FW-MAV). The flapping mechanism was
Externí odkaz:
https://doaj.org/article/c1079d6ec4dd4077957f9e578bb48cb1
Publikováno v:
Journal of Institute of Control, Robotics and Systems. 27:1-10
In this study, proposed is a PD (Proportional-Derivative) controller for the roll and yaw motions based on the linearized and non-coupled lateral mode dynamic model of the flapping-wing micro air vehicle (FW-MAV) called KUBeetle. First, the lateral m
Autor:
Hoang Vu Phan, Hoon Cheol Park
Publikováno v:
Science. 370:1214-1219
Protection in the wings Beetles have hardened forewings for the protection of their bodies and hindwings, and their use during crawling or burrowing is well understood. However, the behavior of the larger hindwings during collisions in flight has not
Publikováno v:
IEEE Robotics and Automation Letters. 5:5059-5066
A hover-capable insect-inspired flying robot that can remain long in the air has shown its potential use for both confined indoor and outdoor applications to complete assigned tasks. In this letter, we report improvements in the flight endurance of o
Publikováno v:
Journal of Institute of Control, Robotics and Systems. 25:960-965
Publikováno v:
International Journal of Micro Air Vehicles. Jan-Dec2019, Vol. 11, p1-10. 10p.
Publikováno v:
Bioinspirationbiomimetics. 15(5)
In this study, the stable proportional-derivative (PD) controller gains for pitch control (longitudinal control) are obtained using the linearized and non-coupled longitudinal-mode flight dynamics model of the tailless, hover-capable, flapping wing r
Publikováno v:
Aerospace Science and Technology. 119:107085
In this paper, we compare the characteristics of hovering stability for two insect-inspired flapping-wing micro air vehicles (FW-MAVs) with different strategies to generate control moments for the longitudinal and lateral attitude controls. The two r
Publikováno v:
Aerospace Science and Technology. 118:106990
A flapping-wing micro air vehicle (FW-MAV) operating with aerodynamically optimal wing configuration and kinematics may save energy and thus prolong flight time. In this work, we use a computational-fluid-dynamic method to investigate the effects of