Development of a morphing helicopter blade with electrochemical actuators by Tubilla Kuri, Fernando

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Real-time embedded sensor processing for an autonomous helicopter by Han, Chin San, 1974-

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Surge dynamics of a helicopter engine gas generator by Corn, Brian A., 1971-

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Experimental investigation of the transient response in pitch of a helicopter by Mallen, Joseph

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Design and control of an autonomous variable-pitch quadrotor helicopter by Cutler, Mark Johnson

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Design of an improved piezoelectric actuator for helicopter rotor control by Tzianetopoulou, Theodora, 1974-

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The instrumentation and system identification for a small agile helicopter by Shterenberg, Alex, 1976-

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Trade study methodology for a helicopter modernization program by Ambrose, Michael H. (Michael Harold), 1961-

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Identification of the harmonic transfer functions of a helicopter rotor by Siddiqi, Afreen, 1977-

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Development of Android phone based controller for RC helicopter by Goh, Jian Hui.

“…The objective of this project is to develop a Smartphone based remote control system to control as well as to include additional features for off-shelf Radio Controlled (RC) Helicopter. Controlling the RC helicopter using the provided controller that comes with the unit may not be the most convenient as it has limitations such as the bulkiness of the controller and the lack of more user friendly interface. …”
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Computational fluid dynamics of helicopter engine exhaust outflow by Chan, Kenneth Mun Chew

“…This paper reviews the computational study of the flow of exhaust gases in a helicopter’s Lobed Mixer Ejector or simply, an exhaust tailpipe. …”
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Classification of helicopters for passive radar - theoretical studies and measurements by Qiao, Na

“…This paper focus on the classification of helicopters for passive bistatic radar. The model of rotating blades has been established based on the mechanism of rotation. …”
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H∞ robust controller for autonomous helicopter hovering control by Tijani, Ismaeel, Akmeliawati, Rini, Legowo, Ari, Budiyono, Agus, Asan Gani, Abdul Muthalif

“…Among the major challenges associated with the deployment of autonomous small scale helicopters in civilian UAV applications is the requirement for reliable control scheme. …”
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Effectiveness of Safety Management Systems of two helicopter operators by Ariffin, Mohd. Adzmi

“…The objective of this study is to determine whether there is any impact in implanting a Safety Management System in helicopter operations. The function of the system is to assist managers: to analyse, to develop, to communicate and to monitor safety at workplace. …”
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UPM airbus helicopters Malaysia meterai MoU by Juferi, Noor Eszereen

“…SERDANG, 28 April – Pusat Penyelidikan Pembuatan Aeroangkasa (AMRC), Universiti Putra Malaysia (UPM) menjalinkan kerjasama bersama AIRBUS Helicopters Malaysia (AHM) Sdn. Bhd. melalui Perjanjian Persefahaman (MoU) ke arah meningkatkan lagi kualiti penyelidikan dan proses pengajaran dan pembelajaran khususnya di UPM dalam bidang aeroangkasa…”
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Effect of surface roughness on helicopter main rotor blade by W. N., W. Rohizan, Mohd.Rafie, Azmin Shakrine, Harmin, Mohammad Yazdi, Ciang, Chia Chen

Subjects: “…Effect of surface roughness; Helicopter; Main rotor blade…”
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UPM, Airbus helicopters Malaysia ink MoU by Juferi, Noor Eszereen

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Effect of surface roughness on helicopter main rotor blade by Wan Rohizan, Wan Norhafizan

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Development Of The Adjustable Engine Mount For The Ultra-Light Helicopter by Azhar, Nur Zhafirah

“…The purpose of this thesis is to design, analyze and fabricate an adjustable engine mount for an ultra-light helicopter. The engine mount must be able to support the load of ROTAX 582 UL DCDI engine and the engine gearbox system which in total is about 70 kg. …”
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Strenght And Stress Analysis On Helicopter Rotor Blade Grip by Sulaiman, Zularieff Redzwan

“…The purpose of this thesis is to design, analyze and apply a spacer with a different materials to the unfilled gap of rotor blade grip for an ultra-light helicopter. The unfilled gap of the blade grip has to be occupied by the spacer in order to obtain the highest grip effectiveness towards the rotor blade. …”
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