Arıkan, Kutluk Bilge

Profile Picture
Profile URL
https://hdl.handle.net/20.500.14411/8140
Name Variants
K.B.Arikan
Kutluk Bilge, Arıkan
K., Arikan
Arıkan,K.B.
Arıkan, Kutluk Bilge
K.B.Arıkan
Kutluk Bilge, Arikan
Arikan, Kutluk Bilge
K.,Arıkan
A., Kutluk Bilge
Arikan,K.B.
A.,Kutluk Bilge
Arikan, K. B.
Job Title
Doktor Öğretim Üyesi
Email Address
kutluk.arikan@atilim.edu.tr
Main Affiliation
Department of Mechatronics Engineering
Status
Former Staff
Website
ORCID ID
Scopus Author ID
Turkish CoHE Profile ID
Google Scholar ID
WoS Researcher ID

Sustainable Development Goals

NO POVERTY1
NO POVERTY
1
Research Products
ZERO HUNGER2
ZERO HUNGER
0
Research Products
GOOD HEALTH AND WELL-BEING3
GOOD HEALTH AND WELL-BEING
1
Research Products
QUALITY EDUCATION4
QUALITY EDUCATION
0
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GENDER EQUALITY5
GENDER EQUALITY
0
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CLEAN WATER AND SANITATION6
CLEAN WATER AND SANITATION
0
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AFFORDABLE AND CLEAN ENERGY7
AFFORDABLE AND CLEAN ENERGY
0
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DECENT WORK AND ECONOMIC GROWTH8
DECENT WORK AND ECONOMIC GROWTH
0
Research Products
INDUSTRY, INNOVATION AND INFRASTRUCTURE9
INDUSTRY, INNOVATION AND INFRASTRUCTURE
1
Research Products
REDUCED INEQUALITIES10
REDUCED INEQUALITIES
0
Research Products
SUSTAINABLE CITIES AND COMMUNITIES11
SUSTAINABLE CITIES AND COMMUNITIES
1
Research Products
RESPONSIBLE CONSUMPTION AND PRODUCTION12
RESPONSIBLE CONSUMPTION AND PRODUCTION
0
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CLIMATE ACTION13
CLIMATE ACTION
0
Research Products
LIFE BELOW WATER14
LIFE BELOW WATER
0
Research Products
LIFE ON LAND15
LIFE ON LAND
0
Research Products
PEACE, JUSTICE AND STRONG INSTITUTIONS16
PEACE, JUSTICE AND STRONG INSTITUTIONS
0
Research Products
PARTNERSHIPS FOR THE GOALS17
PARTNERSHIPS FOR THE GOALS
0
Research Products
This researcher does not have a Scopus ID.
This researcher does not have a WoS ID.
Scholarly Output

38

Articles

11

Views / Downloads

238/2968

Supervised MSc Theses

14

Supervised PhD Theses

7

WoS Citation Count

159

Scopus Citation Count

208

Patents

0

Projects

0

WoS Citations per Publication

4.18

Scopus Citations per Publication

5.47

Open Access Source

3

Supervised Theses

21

JournalCount
Journal of Petroleum Science and Engineering2
20th Annual International Conference on Mechatronics and Machine Vision in Practice, M2VIP 2013 -- 20th Annual International Conference on Mechatronics and Machine Vision in Practice, M2VIP 2013 -- 20 September 2013 through 20 September 2013 -- Ankara -- 1022762
Adaptive Behavior1
AIAA Modeling and Simulation Technologies Conference, 2016 -- AIAA Modeling and Simulation Technologies Conference, 2016 -- 13 June 2016 through 17 June 2016 -- Washington -- 1764991
AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting -- 55th AIAA Aerospace Sciences Meeting -- 9 January 2017 through 13 January 2017 -- Grapevine -- 1264231
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COAR Resource Type: text::conference output

Scholarly Output Search Results

Now showing 1 - 5 of 5
  • Thumbnail Image
    Conference Object
    Citation - WoS: 12
    Design of a Robotic Bicopter
    (Ieee, 2019) Albayrak, Ozge Beyza; Ersan, Yagmur; Bagbasi, Aysen Suheyla; Basaranoglu, Ahmet Turgut; Arikan, Kutluk Bilge
    This article presents a Bicopter type of a flying robot with two rotary-wing units which are placed in a tandem form on the chassis. The rotors are tilted by the aid of the tilt mechanism. Cascaded type of PID controllers are designed on the dynamical models for the attitude and altitude dynamics. The simulated control systems are implemented and tuned on the Naze32 flight controller which is connected to a Raspberry Pi single board computer for real-time applications. The real-time performance is monitored and evaluated during the tests and it is seen that the system is suitable for indoor type of robotic applications.
  • Thumbnail Image
    Conference Object
    Citation - Scopus: 15
    Attitude and Altitude Stabilization of a Fixed Wing Vtol Unmanned Air Vehicle
    (American Institute of Aeronautics and Astronautics Inc, AIAA, 2016) Güçlü,A.; Arıkan,K.B.; Kurtuluş,D.F.
    The aim of the current study is to introduce an overview about the design, manufacturing and testing of a Hybrid Air Vehicle (HAV). The designed vehicle will have the ability to vertically takeoff and landing in addition to fly horizontally as a fixed wing aircraft. A remotely piloted model aircraft (E-Flite Apprentice Model Plane) is selected for the initial tests and it is modified for the current purpose. A thrust measurement setup is used to obtain the thrust characteristics of the motors which are used in the model aircraft for system identification. Another test stand is also designed and manufactured to test the servo motor responses at the control surfaces of the HAV. Inertia tensor of the HAV is obtained experimentally by means of bifilar pendulum test method. The wing of the aircraft will be tested in the 1m x 1mtest section wind tunnel of Aerospace Engineering Department of METU to obtain aerodynamic characteristics. By means of experimentally identified system parameters, the HAV is modeled in Matlab/Simulink environment mathematically. The HAV has three main operating modes such as vertical takeoff and landing, transition to fixed wing flight or vice versa, and fixed wing flight. Combinations of a Linear Active Disturbance Rejection Controller (LADRC) and a Proportional Integral Derivative (PID) based control topologies will be designed for operating modes. To observe performance and enhance the developed system models and controllers, hardware in the loop tests will be done by means of a Flight Motion Simulator (FMS) of ROKETSAN Missile Inc. © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
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    Conference Object
    Disturbance Rejection Control of a Quadrotor Equipped With a 2 Dof Manupilator
    (2013) Aydemir,M.; Arikan,K.B.; Irfanoǧlu,B.
    In this study Active Disturbance Rejection Control (ADRC) is implemented for the attitude dynamics of the quadrotor flying platform. Quadrotor model with a 2 DOF manipulator is constructed. External disturbances, manipulator dynamics and internal plant dynamics are treated as total disturbance which are estimated and rejected in simulation environment.
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    Conference Object
    Citation - Scopus: 2
    Experimental and Numerical Results of a Flapping Wing Four Bar Mechanism
    (American Institute of Aeronautics and Astronautics Inc., 2017) Senol,M.G.; Arikan,K.B.; Kurtulus,D.F.
    This paper explores the design and testing of a flapping wing four-bar mechanism. A four-bar linkage system kinematic analysis is introduced for flapping wing motion. Four-bar mechanism is activated by a servo motor which is driven by microcontroller. The wing undergoes a pure flapping motion at a fixed pitch angle. Force measurements are performed for hover mode by using a force transducer. In addition, 3D numerical analyses are performed and the results are compared with the experimental measurements. Overall, CFD results show good agreement with the experimental data. © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
  • Thumbnail Image
    Conference Object
    Development of a single degree of freedom inertial measurement system
    (2013) Kara,S.E.; Golmohammedzadeh,H.; Arikan,K.B.
    A test bench is designed to develop an inertial measurement unit. Micro electromechanical system (MEMS) type gyro and accelerometer sensors are placed on a rotating platform. Actual angular position is measured by an encoder. This paper presents design of various estimators to estimate the orientation of the test platform. Basically complementary and Kalman filter based estimators are designed and implemented on the test bench. Parameters of the estimators are optimized by using experimental data. Satisfactory results are achieved.