Year 2020, Volume , Issue 18, Pages 738 - 742 2020-04-15

Anfis Based Thrust Estimation of a Small Rotary Wing Drone
Anfis Based Thrust Estimation of a Small Rotary Wing Drone

Hüseyin ŞAHİN [1] , Tugrul OKTAY [2] , Mehmet KONAR [3]


Unmanned Aerial Vehicles (UAV) has an increasingly application for military and civilian fields. Currently, UAVs can perform many tasks such as search-rescue, surveillance by safely. UAVs are specifically designed for their using purpose. The designs of UAVs are an important and long process. It is necessary to evaluate many parameters in the thrust system design. Because of thrust system is the most important system of UAVs. Traditional thrust system design is a trial and error method that is costly and ineffective. In this study, we examined that uav which use brushless motor in thrust system. The force generated by the thrust system has been estimated by using the Adaptive Neuro-Fuzzy Inference System (ANFIS). In the ANFIS model, the thrust force estimation was made by using propeller and motor information. RCbenchmark 1580 model dynamometer was used to measure the accuracy of the ANFIS estimates. Mean square error (MSE) was used to compare test data and ANFIS model. Low MSE ratio shows that ANFIS model is near to real data.
Unmanned Aerial Vehicles (UAV) has an increasingly application for military and civilian fields. Currently, UAVs can perform many tasks such as search-rescue, surveillance by safely. UAVs are specifically designed for their using purpose. The designs of UAVs are an important and long process. It is necessary to evaluate many parameters in the thrust system design. Because of thrust system is the most important system of UAVs. Traditional thrust system design is a trial and error method that is costly and ineffective. In this study, we examined that uav which use brushless motor in thrust system. The force generated by the thrust system has been estimated by using the Adaptive Neuro-Fuzzy Inference System (ANFIS). In the ANFIS model, the thrust force estimation was made by using propeller and motor information. RCbenchmark 1580 model dynamometer was used to measure the accuracy of the ANFIS estimates. Mean square error (MSE) was used to compare test data and ANFIS model. Low MSE ratio shows that ANFIS model is near to real data.
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Primary Language en
Subjects Engineering
Journal Section Articles
Authors

Orcid: 0000-0003-0464-2644
Author: Hüseyin ŞAHİN (Primary Author)
Institution: ANKARA YILDIRIM BEYAZIT ÜNİVERSİTESİ
Country: Turkey


Orcid: 0000-0003-4860-2230
Author: Tugrul OKTAY
Institution: ERCİYES ÜNİVERSİTESİ
Country: Turkey


Orcid: 0000-0002-9317-1196
Author: Mehmet KONAR
Institution: ERCİYES ÜNİVERSİTESİ
Country: Turkey


Dates

Publication Date : April 15, 2020

APA Şahi̇n, H , Oktay, T , Konar, M . (2020). Anfis Based Thrust Estimation of a Small Rotary Wing Drone . Avrupa Bilim ve Teknoloji Dergisi , (18) , 738-742 . DOI: 10.31590/ejosat.694721