-
61
-
62
Feedback controller and observer design to maximize stability radius
Published 2006Get full text
Proceeding Paper -
63
-
64
-
65
Tooth wear and erosive tooth wear among 16-year-old Malaysian adolescents
Published 2013Get full text
Article -
66
Tolerance towards sensor failures: an application to a double inverted pendulum
Published 2006Get full text
Proceeding Paper -
67
Roll and yaw stabilisation using nonlinear energy method
Published 2007Get full text
Proceeding Paper -
68
Automatic aircraft landing control using nonlinear energy method
Published 2010Get full text
Get full text
Proceeding Paper -
69
Disturbance decoupled fault reconstruction using sliding mode observers
Published 2010Get full text
Article -
70
-
71
Disturbance decoupled fault reconstruction using sliding mode observers
Published 2008Get full text
Proceeding Paper -
72
Preliminary design of sliding mode controller for angular positional tracking of an aircraft
Published 2009Get full text
Proceeding Paper -
73
-
74
-
75
Evolution of NACA23012 wake vortices structure using PIV
Published 2012“…The formation and development of a wing‐tip vortex in a near and extended near field were studied experimentally. …”
Get full text
Article -
76
Design of a planar structure of multifrequency patch antenna
Published 2008“…The proposed antenna structure comprises a center patch antenna known as driven patch and two adjacent microstrip patches defined as wing patches. The effect of gap between driven patch and the wing patches have been studied for multiband frequency operation. …”
Get full text
Article -
77
Span load modification via differential spoiler setting
Published 2010“…The serious impact of the wing tips vortices of a large aircraft is well known. …”
Get full text
Proceeding Paper -
78
Stabilty derivatives in the newtonian limit
Published 2013“…They are applicable for wings of arbitrary plan form shape at high angles of attack provided the shock wave is attached to the leading edge of the wing. …”
Get full text
Article -
79
Investigation of Empennage Location Effect to the Unmanned Aerial Vehicle (UAV) Structure Characteristic
Published 2024“…Interestingly, the hybridization of fixed-wing and rotary UAV gives better performance in terms of energy consumption and the needs of runaway. …”
Get full text
Article -
80
Investigation of aerodynamic parameters of a hybrid airship
Published 2012“…The aerodynamic parameters of a preliminary winged-hull airship design are investigated. The research methodology involved the use of numerical simulation and wind tunnel testing. …”
Get full text
Article