TY - GEN
T1 - Development of UGS-TUM Vertical Take off Landing (VTOL) Drone with Flight Control
AU - Wan, Andre Novianto
AU - Sim, Glendon Mao Shen
AU - Koh, Ryan Wee Lun
AU - Koh, Ryan Kok Fong
AU - Teo, Gibson Tubiba
AU - Yap, Thian Hong
AU - Nilju, Tin
AU - Srigrarom, Sutthiphong
AU - Holzapfel, Florian
AU - Marvakov, Valentin
AU - Bhadwaj, Pranav
AU - Tantrairatn, Suradet
AU - Sakulthong, Sarul
N1 - Publisher Copyright:
© 2019 IEEE.
PY - 2019/2/20
Y1 - 2019/2/20
N2 - This paper presents the design of a fixed-wing Vertical Take-off and Landing (VTOL) UAV 'Black Wing' Tiltrotor for the transition to forward flight. With fixed-wing VTOL aircraft can achieve longer flight time and range and able take-off/land at any terrain without runways. The design of the fixed-wing VTOL UAV will consist of four motors similar to a quadcopter after take-off to a certain altitude the front two the motors will slowly tilt to almost 90 degrees for forwarding flight. The focus is on the study of the manoeuvre flight characteristics, such as the roll, pitch, yaw and elevation control input and output of the fixed-wing VTOL UAV. MATLAB and Simulink will be used to develop a control system by using the equation of motion (EOM). This paper also gives a better understanding of how the fixed-wing VTOL UAV works, how it transits from quad mode to a wing-borne forward flight mode while utilising the tilt rotors.
AB - This paper presents the design of a fixed-wing Vertical Take-off and Landing (VTOL) UAV 'Black Wing' Tiltrotor for the transition to forward flight. With fixed-wing VTOL aircraft can achieve longer flight time and range and able take-off/land at any terrain without runways. The design of the fixed-wing VTOL UAV will consist of four motors similar to a quadcopter after take-off to a certain altitude the front two the motors will slowly tilt to almost 90 degrees for forwarding flight. The focus is on the study of the manoeuvre flight characteristics, such as the roll, pitch, yaw and elevation control input and output of the fixed-wing VTOL UAV. MATLAB and Simulink will be used to develop a control system by using the equation of motion (EOM). This paper also gives a better understanding of how the fixed-wing VTOL UAV works, how it transits from quad mode to a wing-borne forward flight mode while utilising the tilt rotors.
KW - AAVC 2018
KW - Fixed-wing Vertical Take Off Landing (VTOL) UAV
KW - Tiltrotor
UR - http://www.scopus.com/inward/record.url?scp=85063249665&partnerID=8YFLogxK
U2 - 10.1109/ICA-SYMP.2019.8646176
DO - 10.1109/ICA-SYMP.2019.8646176
M3 - Conference contribution
AN - SCOPUS:85063249665
T3 - 2019 1st International Symposium on Instrumentation, Control, Artificial Intelligence, and Robotics, ICA-SYMP 2019
SP - 213
EP - 221
BT - 2019 1st International Symposium on Instrumentation, Control, Artificial Intelligence, and Robotics, ICA-SYMP 2019
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 1st International Symposium on Instrumentation, Control, Artificial Intelligence, and Robotics, ICA-SYMP 2019
Y2 - 16 January 2019 through 18 January 2019
ER -