TY - GEN
T1 - Tri-Tilting Rotor Fixed-Wing VTOL UAV
T2 - 2021 International Symposium on Electrical, Electronics and Information Engineering, ISEEIE 2021
AU - Hegde, Navya Thirumaleshwar
AU - George, V. I.
AU - Gurudas Nayak, C.
N1 - Funding Information:
The authors convey their gratitude to the Dept. of ICE, MIT, MAHE, Manipal, for permitting the research to be conducted in their laboratory and providing the necessary facilities. The authors significantly appreciate the anonymous referees and the editor's positive and valuable comments that have improved the quality of this research article.
Publisher Copyright:
© 2021 ACM.
PY - 2021/2/19
Y1 - 2021/2/19
N2 - This paper gives the dynamic modeling and design of a controller for autonomous Vertical take-off and landing (VTOL) Tri-Tilt rotor hybrid Unmanned Aerial Vehicle (UAV). Nowadays, UAVs have experienced remarkable progress and mainly categorized into fixed-wing UAVs and rotary-wing UAVs. The Tri Tiltrotor UAV models are derived mathematically using Euler's force and moment equations for VTOL to horizontal flight and vice-versa using MATLAB. The development of fully autonomous and self-guided UAVs would reduce the risk to human life. The applications consist of inspection of coasts, terrain, border, patrol buildings, rescue teams, police, and pipelines. A Proportional-Integral-Derivative control method is proposed for UAVs attitude and altitude stabilization. The results reveal that the controller accomplishes adaptability, robust performance and stability in the transition mode.
AB - This paper gives the dynamic modeling and design of a controller for autonomous Vertical take-off and landing (VTOL) Tri-Tilt rotor hybrid Unmanned Aerial Vehicle (UAV). Nowadays, UAVs have experienced remarkable progress and mainly categorized into fixed-wing UAVs and rotary-wing UAVs. The Tri Tiltrotor UAV models are derived mathematically using Euler's force and moment equations for VTOL to horizontal flight and vice-versa using MATLAB. The development of fully autonomous and self-guided UAVs would reduce the risk to human life. The applications consist of inspection of coasts, terrain, border, patrol buildings, rescue teams, police, and pipelines. A Proportional-Integral-Derivative control method is proposed for UAVs attitude and altitude stabilization. The results reveal that the controller accomplishes adaptability, robust performance and stability in the transition mode.
UR - https://www.scopus.com/pages/publications/85113215208
UR - https://www.scopus.com/pages/publications/85113215208#tab=citedBy
U2 - 10.1145/3459104.3459118
DO - 10.1145/3459104.3459118
M3 - Conference contribution
AN - SCOPUS:85113215208
T3 - ACM International Conference Proceeding Series
SP - 66
EP - 71
BT - Proceedings - 2021 International Symposium on Electrical, Electronics and Information Engineering, ISEEIE 2021
PB - Association for Computing Machinery, Inc
Y2 - 19 February 2021 through 21 February 2021
ER -