TY - GEN
T1 - Tailsitter VTOL flying wing aircraft attitude control
AU - Liang, Jianjian
AU - Fei, Qing
AU - Wang, Bo
AU - Geng, Qingbo
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2017/1/3
Y1 - 2017/1/3
N2 - This paper introduces a flying-wing tail-sitter aircraft which can switch between vertical flight mode (rotary-wing mode) and level flight mode (fixed-wing mode). Equipped with two propellers and two elevons, the aircraft can fly by controlling these four actuators. The aircraft uses a microcomputer and various sensors to stabilize the attitude and to switch modes on command. Using the transition logic, it can receive and act on the signal sent by operator at any time, whether it is to switch modes or to retract the command. Using the target angle calculation algorithm, the aircraft can adjust its pitch angle during transition. PID feedback is used for attitude control both in vertical mode and during the transition. Test results show that the aircraft have the advantages of helicopters and fix-wing airplanes. It can hover midair and does not need runway to take off, and it can fly in high speed in fixed-wing mode.
AB - This paper introduces a flying-wing tail-sitter aircraft which can switch between vertical flight mode (rotary-wing mode) and level flight mode (fixed-wing mode). Equipped with two propellers and two elevons, the aircraft can fly by controlling these four actuators. The aircraft uses a microcomputer and various sensors to stabilize the attitude and to switch modes on command. Using the transition logic, it can receive and act on the signal sent by operator at any time, whether it is to switch modes or to retract the command. Using the target angle calculation algorithm, the aircraft can adjust its pitch angle during transition. PID feedback is used for attitude control both in vertical mode and during the transition. Test results show that the aircraft have the advantages of helicopters and fix-wing airplanes. It can hover midair and does not need runway to take off, and it can fly in high speed in fixed-wing mode.
KW - Attitude control
KW - flight mode transition
KW - vertical takeoff and landing
UR - http://www.scopus.com/inward/record.url?scp=85011030482&partnerID=8YFLogxK
U2 - 10.1109/YAC.2016.7804934
DO - 10.1109/YAC.2016.7804934
M3 - Conference contribution
AN - SCOPUS:85011030482
T3 - Proceedings - 2016 31st Youth Academic Annual Conference of Chinese Association of Automation, YAC 2016
SP - 439
EP - 443
BT - Proceedings - 2016 31st Youth Academic Annual Conference of Chinese Association of Automation, YAC 2016
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 31st Youth Academic Annual Conference of Chinese Association of Automation, YAC 2016
Y2 - 11 November 2016 through 13 November 2016
ER -