TY - GEN
T1 - Ugs-sit-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, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - This paper presents the design a fixed-wing Vertical Take-off and Landing (VTOL) UAV with 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 a fixed-wing Vertical Take-off and Landing (VTOL) UAV with 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 - Autonomous Aerial Vehicle Challenge (AAVC)
KW - — Fixed-wing Vertical Take Off & Landing (VTOL) UAV
UR - http://www.scopus.com/inward/record.url?scp=85099120086&partnerID=8YFLogxK
U2 - 10.2514/6.2019-3140
DO - 10.2514/6.2019-3140
M3 - Conference contribution
AN - SCOPUS:85099120086
SN - 9781624105890
T3 - AIAA Aviation 2019 Forum
SP - 1
EP - 14
BT - AIAA Aviation 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation 2019 Forum
Y2 - 17 June 2019 through 21 June 2019
ER -