Haithem E. Taha
Haithem E. Taha
Professor of Mechanical and Aerospace Engineering, University of California, Irvine
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Zitiert von
Zitiert von
State-space representation of the unsteady aerodynamics of flapping flight
HE Taha, MR Hajj, PS Beran
Aerospace Science and Technology 34, 1-11, 2014
Flight dynamics and control of flapping-wing MAVs: a review
HE Taha, MR Hajj, AH Nayfeh
Nonlinear Dynamics 70, 907-939, 2012
The need for higher-order averaging in the stability analysis of hovering, flapping-wing flight
HE Taha, S Tahmasian, CA Woolsey, AH Nayfeh, MR Hajj
Bioinspiration & biomimetics 10 (1), 016002, 2015
Vibrational control: A hidden stabilization mechanism in insect flight
HE Taha, M Kiani, TL Hedrick, JSM Greeter
Science robotics 5 (46), eabb1502, 2020
Optimal morphing–augmented dynamic soaring maneuvers for unmanned air vehicle capable of span and sweep morphologies
I Mir, A Maqsood, SA Eisa, H Taha, S Akhtar
Aerospace Science and Technology 79, 17-36, 2018
Longitudinal flight dynamics of hovering MAVs/insects
HE Taha, MR Hajj, AH Nayfeh
Journal of Guidance, Control, and Dynamics 37 (3), 970-979, 2014
Viscous extension of potential-flow unsteady aerodynamics: the lift frequency response problem
H Taha, AS Rezaei
Journal of Fluid Mechanics 868, 141-175, 2019
A controllability perspective of dynamic soaring
I Mir, H Taha, SA Eisa, A Maqsood
Nonlinear Dynamics 94, 2347-2362, 2018
Wing kinematics optimization for hovering micro air vehicles using calculus of variation
HE Taha, MR Hajj, AH Nayfeh
Journal of Aircraft 50 (2), 610-614, 2013
Geometrically-exact unsteady model for airfoils undergoing large amplitude maneuvers
Z Yan, HE Taha, MR Hajj
Aerospace Science and Technology 39, 293-306, 2014
On higher-order averaging of time-periodic systems: reconciliation of two averaging techniques
M Maggia, SA Eisa, HE Taha
Nonlinear Dynamics 99, 813-836, 2020
Geometric control approach to longitudinal stability of flapping flight
HE Taha, CA Woolsey, MR Hajj
Journal of Guidance, Control, and Dynamics 39 (2), 214-226, 2016
Nonlinear characteristics of an autoparametric vibration system
Z Yan, HE Taha, T Tan
Journal of sound and vibration 390, 1-22, 2017
Measurement and modeling of lift enhancement on plunging airfoils: A frequency response approach
MY Zakaria, HE Taha, MR Hajj
Journal of Fluids and Structures 69, 187-208, 2017
Effect of the aerodynamic-induced parametric excitation on the longitudinal stability of hovering MAVs/insects
HE Taha, AH Nayfeh, MR Hajj
Nonlinear Dynamics 78, 2399-2408, 2014
Soaring energetics for a nature inspired unmanned aerial vehicle
I Mir, A Maqsood, HE Taha, SA Eisa
AIAA Scitech 2019 Forum, 1622, 2019
Differential-geometric-control formulation of flapping flight multi-body dynamics
AM Hassan, HE Taha
Journal of Nonlinear Science 29, 1379-1417, 2019
Design optimization of flapping ornithopters: The pterosaur replica in forward flight
MY Zakaria, HE Taha, MR Hajj
Journal of Aircraft 53 (1), 48-59, 2016
Effects of aerodynamic modeling on the optimal wing kinematics for hovering MAVs
Z Yan, HE Taha, MR Hajj
Aerospace Science and Technology 45, 39-49, 2015
A stability perspective of bioinspired unmanned aerial vehicles performing optimal dynamic soaring
I Mir, SA Eisa, H Taha, A Maqsood, S Akhtar, TU Islam
Bioinspiration & Biomimetics 16 (6), 066010, 2021
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