Altınuç, Kemal Orçun

Profile Picture
Profile URL
https://hdl.handle.net/20.500.14411/7100
Name Variants
Kemal Orçun, Altınuç
K., Altinuc
K.,Altınuç
A., Kemal Orçun
Altınuç, Kemal Orçun
K. O. Altınuç
Kemal Orcun, Altinuc
K.O.Altinuc
Altinuç, Kemal Orçun
Altinuc,K.O.
A.,Kemal Orçun
K. O. Altinuc
Altınuç,K.O.
A., Kemal Orcun
Altinuc, Kemal Orcun
K.,Altinuç
Kemal Orçun, Altinuç
K. O. Altinuç
K.O.Altınuç
A.,Kemal Orcun
Job Title
Araştırma Görevlisi
Email Address
orcun.altinuc@atilim.edu.tr
Main Affiliation
Mechatronics Engineering
Status
Website
ORCID ID
Scopus Author ID
Turkish CoHE Profile ID
Google Scholar ID
WoS Researcher ID
HTA-9049-2023

Sustainable Development Goals

SDG data is not available
This researcher does not have a Scopus ID.
Documents

2

Citations

5

Go to WoS profile
Scholarly Output

3

Articles

1

Views / Downloads

17/389

Supervised MSc Theses

1

Supervised PhD Theses

0

WoS Citation Count

5

Scopus Citation Count

6

Patents

0

Projects

0

WoS Citations per Publication

1.67

Scopus Citations per Publication

2.00

Open Access Source

1

Supervised Theses

1

JournalCount
32nd IEEE Signal Processing and Communications Applications Conference (SIU) -- MAY 15-18, 2024 -- Tarsus Univ Campus, Mersin, TURKEY1
PLOS ONE1
Current Page: 1 / 1

Scopus Quartile Distribution

Competency Cloud

GCRIS Competency Cloud

Filters

20231
Reset filters

Settings

COAR Resource Type: text::journal::journal article

Scholarly Output Search Results

Now showing 1 - 1 of 1
  • Thumbnail Image
    Article
    Citation - WoS: 5
    Citation - Scopus: 4
    Avoiding Contingent Incidents by Quadrotors Due To One or Two Propellers Failure
    (Public Library Science, 2023) Altinuc, Kemal Orcun; Khan, Muhammad Umer; Iqbal, Jamshed
    With the increasing impact of drones in our daily lives, safety issues have become a primary concern. In this study, a novel supervisor-based active fault-tolerant (FT) control system is presented for a rotary-wing quadrotor to maintain its pose in 3D space upon losing one or two propellers. Our approach allows the quadrotor to make controlled movements about a primary axis attached to the body-fixed frame. A multi-loop cascaded control architecture is designed to ensure robustness, stability, reference tracking, and safe landing. The altitude control is performed using a proportional-integral-derivative (PID) controller, whereas linear-quadratic-integral (LQI) and model-predictive-control (MPC) have been investigated for reduced attitude control and their performance is compared based on absolute and mean-squared error. The simulation results affirm that the quadrotor remains in a stable region, successfully performs the reference tracking, and ensures a safe landing while counteracting the effects of propeller(s) failures.