TY - GEN
T1 - Flight transition control of a multipurpose UAV
AU - Vorsin, David
AU - Arogeti, Shai
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/8/4
Y1 - 2017/8/4
N2 - This paper describes the design and control approach of a new vertical takeoff and landing (VTOL) unmanned aerial vehicles (UAV), capable of a plane-like horizontal flight. The UAV design includes dynamical modeling, control design and implementation. The main control challenge with this UAV stems from the complicated and unpredicted behavior of the vehicle during flight state transitions. This paper suggests a safe and efficient transition approach, between horizontal and vertical flights, which is demonstrated trough simulations and experiments. Additionally, real flight tests show that the UAV is capable of both stable hovering and efficient horizontal flight.
AB - This paper describes the design and control approach of a new vertical takeoff and landing (VTOL) unmanned aerial vehicles (UAV), capable of a plane-like horizontal flight. The UAV design includes dynamical modeling, control design and implementation. The main control challenge with this UAV stems from the complicated and unpredicted behavior of the vehicle during flight state transitions. This paper suggests a safe and efficient transition approach, between horizontal and vertical flights, which is demonstrated trough simulations and experiments. Additionally, real flight tests show that the UAV is capable of both stable hovering and efficient horizontal flight.
UR - http://www.scopus.com/inward/record.url?scp=85029894255&partnerID=8YFLogxK
U2 - 10.1109/ICCA.2017.8003112
DO - 10.1109/ICCA.2017.8003112
M3 - Conference contribution
AN - SCOPUS:85029894255
T3 - IEEE International Conference on Control and Automation, ICCA
SP - 507
EP - 512
BT - 2017 13th IEEE International Conference on Control and Automation, ICCA 2017
PB - Institute of Electrical and Electronics Engineers
T2 - 13th IEEE International Conference on Control and Automation, ICCA 2017
Y2 - 3 July 2017 through 6 July 2017
ER -