TY - GEN
T1 - Modeling and Multimode Analysis of Electrically Driven Flying Car
AU - Ai, Tianfu
AU - Xu, Bin
AU - Xiang, Changle
AU - Fan, Wei
AU - Zhang, Yibo
N1 - Publisher Copyright:
© 2020 IEEE.
PY - 2020/9
Y1 - 2020/9
N2 - Aiming at a flying car which can be used for land-air amphibious, the dynamic models of its land drive module and air flight module are built respectively to obtain the simulation model under different working conditions. In order to ensure that the simulation model can stably track the driving speed and other indicators, different controllers are designed for the land and air modules as the nominal control structures, respectively. A series of simulations of different working conditions for flying car are presented, such as straight-line driving on the ground to fly in the air. The results show that the vehicle can track the speed well under the straight-line driving condition, and it can track the height well under the hovering condition. The vehicle wheel vertical load and lateral load will decrease to zero during switching driving on ground to fly in the air. When it takes off completely, it will experience an oscillation process and finally stabilize.
AB - Aiming at a flying car which can be used for land-air amphibious, the dynamic models of its land drive module and air flight module are built respectively to obtain the simulation model under different working conditions. In order to ensure that the simulation model can stably track the driving speed and other indicators, different controllers are designed for the land and air modules as the nominal control structures, respectively. A series of simulations of different working conditions for flying car are presented, such as straight-line driving on the ground to fly in the air. The results show that the vehicle can track the speed well under the straight-line driving condition, and it can track the height well under the hovering condition. The vehicle wheel vertical load and lateral load will decrease to zero during switching driving on ground to fly in the air. When it takes off completely, it will experience an oscillation process and finally stabilize.
UR - http://www.scopus.com/inward/record.url?scp=85094978668&partnerID=8YFLogxK
U2 - 10.1109/ICUAS48674.2020.9213861
DO - 10.1109/ICUAS48674.2020.9213861
M3 - Conference contribution
AN - SCOPUS:85094978668
T3 - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
SP - 1565
EP - 1571
BT - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
Y2 - 1 September 2020 through 4 September 2020
ER -