TY - JOUR
T1 - Flight Control for UAV Loitering over a Ground Target with Unknown Maneuver
AU - Dong, Fei
AU - You, Keyou
AU - Zhang, Jiaqi
N1 - Publisher Copyright:
© 1993-2012 IEEE.
PY - 2020/11
Y1 - 2020/11
N2 - This article proposes a flight controller for an unmanned aerial vehicle (UAV) to loiter over a ground moving target (GMT). We are concerned with the scenario that the stochastically time-varying maneuver of the GMT is unknown to the UAV, which renders it challenging to estimate the GMT's motion state. Assuming that the state of the GMT is available, we first design a discrete-time Lyapunov vector field for the loitering guidance and then design a discrete-time integral sliding mode control (ISMC) to track the guidance commands. By modeling the maneuver process as a finite-state Markov chain, we propose a Rao-Blackwellised particle filter (RBPF), which only requires a few number of particles, to simultaneously estimate the motion state and the maneuver of the GMT with a camera or radar sensor. Then, we apply the principle of certainty equivalence to the ISMC and obtain the flight controller for completing the loitering task. Finally, the effectiveness and advantages of our controller are validated via simulations.
AB - This article proposes a flight controller for an unmanned aerial vehicle (UAV) to loiter over a ground moving target (GMT). We are concerned with the scenario that the stochastically time-varying maneuver of the GMT is unknown to the UAV, which renders it challenging to estimate the GMT's motion state. Assuming that the state of the GMT is available, we first design a discrete-time Lyapunov vector field for the loitering guidance and then design a discrete-time integral sliding mode control (ISMC) to track the guidance commands. By modeling the maneuver process as a finite-state Markov chain, we propose a Rao-Blackwellised particle filter (RBPF), which only requires a few number of particles, to simultaneously estimate the motion state and the maneuver of the GMT with a camera or radar sensor. Then, we apply the principle of certainty equivalence to the ISMC and obtain the flight controller for completing the loitering task. Finally, the effectiveness and advantages of our controller are validated via simulations.
KW - Ground moving target (GMT) with unknown maneuver
KW - Lyapunov guidance vector field
KW - loitering
KW - particle filter
KW - sliding mode control (SMC)
KW - unmanned aerial vehicle (UAV)
UR - https://www.scopus.com/pages/publications/85085965888
U2 - 10.1109/TCST.2019.2948915
DO - 10.1109/TCST.2019.2948915
M3 - 文章
AN - SCOPUS:85085965888
SN - 1063-6536
VL - 28
SP - 2461
EP - 2473
JO - IEEE Transactions on Control Systems Technology
JF - IEEE Transactions on Control Systems Technology
IS - 6
M1 - 8897108
ER -