TY - GEN
T1 - Finite-time Autonomous Shipboard Landing Control of a Helicopter with Time-varying Output Constraints
AU - Huang, Yanting
AU - Zhu, Ming
AU - Zheng, Zewei
AU - Zhu, Bing
N1 - Publisher Copyright:
© 2019 IEEE.
PY - 2019/7
Y1 - 2019/7
N2 - This paper addresses a finite-time autonomous shipboard landing problem of a model helicopter subject to output constraints, parametric uncertainties and external disturbances. By establishing the relative motion model between the helicopter and the ship, the shipboard landing problem is converted from a general trajectory tracking problem to a stabilization problem. Due to the under-actuated property of the helicopter, the whole process of the autonomous shipboard is divided into two steps. The helicopter is first commanded by a relative position controller (RPC) to reach above the ship. As it reaches, a relative attitude-altitude controller (RAC) is initiated to guide the helicopter to descend steadily on the ship. RPC and RAC are both devised in terms of the tan-type Barrier Lyapunov Function theory, with an adaptive estimation method inserted to compensate for the impact of uncertainties and disturbances. It is demonstrated from the stability analysis that the proposed control strategy can ensure that system tracking errors converge to small sets around zero in the finite time and never violating constraint requirements. Numerical simulations are implemented to further validate the remarkable control performance.
AB - This paper addresses a finite-time autonomous shipboard landing problem of a model helicopter subject to output constraints, parametric uncertainties and external disturbances. By establishing the relative motion model between the helicopter and the ship, the shipboard landing problem is converted from a general trajectory tracking problem to a stabilization problem. Due to the under-actuated property of the helicopter, the whole process of the autonomous shipboard is divided into two steps. The helicopter is first commanded by a relative position controller (RPC) to reach above the ship. As it reaches, a relative attitude-altitude controller (RAC) is initiated to guide the helicopter to descend steadily on the ship. RPC and RAC are both devised in terms of the tan-type Barrier Lyapunov Function theory, with an adaptive estimation method inserted to compensate for the impact of uncertainties and disturbances. It is demonstrated from the stability analysis that the proposed control strategy can ensure that system tracking errors converge to small sets around zero in the finite time and never violating constraint requirements. Numerical simulations are implemented to further validate the remarkable control performance.
UR - https://www.scopus.com/pages/publications/85075786723
U2 - 10.1109/ICCA.2019.8899912
DO - 10.1109/ICCA.2019.8899912
M3 - 会议稿件
AN - SCOPUS:85075786723
T3 - IEEE International Conference on Control and Automation, ICCA
SP - 441
EP - 446
BT - 2019 IEEE 15th International Conference on Control and Automation, ICCA 2019
PB - IEEE Computer Society
T2 - 15th IEEE International Conference on Control and Automation, ICCA 2019
Y2 - 16 July 2019 through 19 July 2019
ER -