Ermira Junita Abdullah

Dr. Ermira Junita Abdullah

Universiti Putra Malaysia (UPM)
orcid

Research Focus & Metrics

Academic Career Length

21Years (2006-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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11 February 2013 in Journal of Intelligent Material Systems and Structures
Verified
Journal Article
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CBCees Bil
Cees Bil
KMKevin Massey
Kevin Massey
EAErmira Junita Abdullah
Ermira Junita Abdullah
Aircraft morphing is referred to as the ability for an aircraft to change its geometry in flight. Formally, flaps, spoilers, and control devices are considered morphing, but in general, morphing in aerospace is associated with geometrical changes using smart materials such as shape memory alloys. Shape memory alloy is a material that changes shape under heating and produces force and deflections, which make it potential actuator for a wing morphing system. The motivation behind this study is the application to small-sized and medium-sized unmanned air vehicles and the potential to increase range or endurance for a given fuel load through improved lift-to-drag ratio. The camber line of an airfoil section, the predominant parameter affecting lift and drag, is changed by resistive heating of a shape memory alloy actuator and cooling in the surrounding air. Experiments were conducted under wind tunnel conditions to verify analysis and to investigate the effects of its application on the aerodynamic behavior of the wing. This study investigated three control methodologies: the conventional proportional–integral–derivative controller, proportional–integral–derivative with robust compensator, and proportional–integral–derivative with anti-windup compensator. The latter proved to have superior performance in achieving and maintaining a required level of morphing. In addition, the power required to the shape memory alloy actuators under aerodynamic load, and the effect of ambient temperature was also investigated.

1 September 2006 in Composite Structures
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Journal Article
Closed access
EME. Mahdi
E. Mahdi
AMA.S. Mokhtar
A.S. Mokhtar
NAN.A. Asari
N.A. Asari
FEF. Elfaki
F. Elfaki
EAErmira Junita Abdullah
Ermira Junita Abdullah

5 January 2009
Verified
Conference Paper
Closed access
EAErmira Junita Abdullah
Ermira Junita Abdullah
CBCees Bil
Cees Bil
SWSimon Watkins
Simon Watkins

27 March 2021 in Drones
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Journal Article
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Javaan ChahlJavaan Chahl
Javaan Chahl
NCNasim Chitsaz
Nasim Chitsaz
BMBlake McIvor
Blake McIvor
TOTitilayo Ogunwa
Titilayo Ogunwa
JKJia-Ming Kok
Jia-Ming Kok
EAErmira Junita Abdullah
Ermira Junita Abdullah
Many drone platforms have matured to become nearly optimal flying machines with only modest improvements in efficiency possible. “Chimera” craft combine fixed wing and rotary wing characteristics while being substantially less efficient than both. The increasing presence of chimeras suggests that their mix of vertical takeoff, hover, and more efficient cruise is invaluable to many end users. We discuss the opportunity for flapping wing drones inspired by large insects to perform these mixed missions. Dragonflies particularly are capable of efficiency in all modes of flight. We will explore the fundamental principles of dragonfly flight to allow for a comparison between proposed flapping wing technological solutions and a flapping wing organism. We chart one approach to achieving the next step in drone technology through systems theory and an appreciation of how biomimetics can be applied. New findings in dynamics of flapping, practical actuation technology, wing design, and flight control are presented and connected. We show that a theoretical understanding of flight systems and an appreciation of the detail of biological implementations may be key to achieving an outcome that matches the performance of natural systems. We assert that an optimal flapping wing drone, capable of efficiency in all modes of flight with high performance upon demand, might look somewhat like an abstract dragonfly.

7 November 2020 in Microsystem Technologies
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Journal Article
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EAErmira Junita Abdullah
Ermira Junita Abdullah
JSJosu Soriano
Josu Soriano
IGIñaki Fernández de Bastida Garrido
Iñaki Fernández de Bastida Garrido
DMDayang Laila Abdul Majid
Dayang Laila Abdul Majid

1 July 2011 in Aerospace Science and Technology
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Journal Article
Closed access
AAA. Attaran
A. Attaran
DMD.L. Majid
D.L. Majid
SBS. Basri
S. Basri
ARA.S. Mohd Rafie
A.S. Mohd Rafie
EAErmira Junita Abdullah
Ermira Junita Abdullah