TY - GEN
T1 - Relative motion modeling and control for a quadrotor landing on an unmanned vessel
AU - Jin, Cheng
AU - Zhu, Ming
AU - Sun, Liang
AU - Zheng, Zewei
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - This paper presents the design of an autopilot for autonomous landing of a quadrotor on an unmanned vessel. The problem of quadrotor landing was usually treated as a trajectory tracking problem, but in this paper, it is converted as a stabilization problem of relative motion to facilitate the controller design. A coupled six-degrees-of-freedom (6-DOF) non- linear relative motion model with four control inputs is established. The landing controller is divided into two parts, relative position controller(RPC) and relative attitude-altitude controller(RAC). RPC is proposed for use when the quadrotor is far away from the vessel, which is aimed at controlling the quadrotor to y to the vicinity of the unmanned vessel.RAC is used for the situation when the quadrotor is close to the vessel, which can control the quadrotor to land on the vessel steadily. To overcome the problem of nonlinear and strong coupling features of the relative system, a backstepping technique is applied in both RPC and RAC. The performance of the autopilot is demonstrated by computer simulations.
AB - This paper presents the design of an autopilot for autonomous landing of a quadrotor on an unmanned vessel. The problem of quadrotor landing was usually treated as a trajectory tracking problem, but in this paper, it is converted as a stabilization problem of relative motion to facilitate the controller design. A coupled six-degrees-of-freedom (6-DOF) non- linear relative motion model with four control inputs is established. The landing controller is divided into two parts, relative position controller(RPC) and relative attitude-altitude controller(RAC). RPC is proposed for use when the quadrotor is far away from the vessel, which is aimed at controlling the quadrotor to y to the vicinity of the unmanned vessel.RAC is used for the situation when the quadrotor is close to the vessel, which can control the quadrotor to land on the vessel steadily. To overcome the problem of nonlinear and strong coupling features of the relative system, a backstepping technique is applied in both RPC and RAC. The performance of the autopilot is demonstrated by computer simulations.
UR - https://www.scopus.com/pages/publications/85086950234
U2 - 10.2514/6.2017-1522
DO - 10.2514/6.2017-1522
M3 - 会议稿件
AN - SCOPUS:85086950234
SN - 9781624104503
T3 - AIAA Guidance, Navigation, and Control Conference, 2017
BT - AIAA Guidance, Navigation, and Control Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Guidance, Navigation, and Control Conference, 2017
Y2 - 9 January 2017 through 13 January 2017
ER -