TY - JOUR
T1 - Prescribed performance tracking control for an unmanned aerial vehicle under desired trajectory attacks
AU - Pan, Kunpeng
AU - Yang, Feisheng
AU - Xia, Juan
AU - Lyu, Yang
N1 - Publisher Copyright:
© 2026 The Franklin Institute. Published by Elsevier Inc. All rights are reserved, including those for text and data mining, AI training, and similar technologies.
PY - 2026/8/1
Y1 - 2026/8/1
N2 - This paper proposes a prescribed performance tracking control method for an unmanned aerial vehicle (UAV) to counteract both desired trajectory attacks and time-varying disturbances. First, an extended state observer is designed to filter position and velocity measurements and to estimate and compensate for security threats such as desired trajectory attacks and external disturbances. Then, under the backstepping framework, the transient and steady-state responses of the position tracking error are constrained using a barrier function. Subsequently, a security controller that incorporates a compensation mechanism -namely, a thrust command law- is derived. The desired attitude angles are then determined. Following this, the attitude tracking controller is designed based on the backstepping method. Finally, simulation results for different scenarios are presented to verify the feasibility of the proposed scheme.
AB - This paper proposes a prescribed performance tracking control method for an unmanned aerial vehicle (UAV) to counteract both desired trajectory attacks and time-varying disturbances. First, an extended state observer is designed to filter position and velocity measurements and to estimate and compensate for security threats such as desired trajectory attacks and external disturbances. Then, under the backstepping framework, the transient and steady-state responses of the position tracking error are constrained using a barrier function. Subsequently, a security controller that incorporates a compensation mechanism -namely, a thrust command law- is derived. The desired attitude angles are then determined. Following this, the attitude tracking controller is designed based on the backstepping method. Finally, simulation results for different scenarios are presented to verify the feasibility of the proposed scheme.
KW - Backstepping method
KW - Desired trajectory attack
KW - Extended state observer
KW - Prescribed performance
KW - Unmanned aerial vehicle
UR - https://www.scopus.com/pages/publications/105041242579
U2 - 10.1016/j.jfranklin.2026.108805
DO - 10.1016/j.jfranklin.2026.108805
M3 - 文章
AN - SCOPUS:105041242579
SN - 0016-0032
VL - 363
JO - Journal of the Franklin Institute
JF - Journal of the Franklin Institute
IS - 12
M1 - 108805
ER -