TY - JOUR
T1 - Piecewise Trajectory and Angle Constraint-Based Fractional-Order Sliding Mode Control
AU - Fan, Junfang
AU - Chen, Shiwei
AU - Wang, Wei
AU - Ji, Yi
AU - Liu, Ning
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2023/10/1
Y1 - 2023/10/1
N2 - This article proposes an approach for piecewise trajectory planning and fractional-order sliding-mode guidance of a two-stage launched miniature munition with the laser beam riding steered guidance technology. In the proposed approach, first, the polynomial description is used as an expected trajectory. Then consider the random external disturbances/parametric uncertainties and other factors deteriorate the tracking control performances of the miniature munition. To reduce the chattering caused by modeling errors and external disturbances and achieve fast speed and high-accuracy tracking performances for miniature munition, based on adaptive multipower reaching strategy, an integrated guidance and control (IGC) method with the fractional-order sliding-mode guidance law (FOSMGL) is introduced. The designed fractional-order sliding surfaces ultimately and successively allow both the trajectory and the attitude angle converge to expected value in a finite time. In addition, considering the case of a moving target, a feedforward compensation mechanism, which decreases the lag of the guidance system, is imposed using an additional compensated term obtained from the attitude angle error. The convergence and reachability of the proposed algorithm in finite-time are analyzed using the Lyapunov function method. The validity and practicability of the proposed method are verified by a numerical example.
AB - This article proposes an approach for piecewise trajectory planning and fractional-order sliding-mode guidance of a two-stage launched miniature munition with the laser beam riding steered guidance technology. In the proposed approach, first, the polynomial description is used as an expected trajectory. Then consider the random external disturbances/parametric uncertainties and other factors deteriorate the tracking control performances of the miniature munition. To reduce the chattering caused by modeling errors and external disturbances and achieve fast speed and high-accuracy tracking performances for miniature munition, based on adaptive multipower reaching strategy, an integrated guidance and control (IGC) method with the fractional-order sliding-mode guidance law (FOSMGL) is introduced. The designed fractional-order sliding surfaces ultimately and successively allow both the trajectory and the attitude angle converge to expected value in a finite time. In addition, considering the case of a moving target, a feedforward compensation mechanism, which decreases the lag of the guidance system, is imposed using an additional compensated term obtained from the attitude angle error. The convergence and reachability of the proposed algorithm in finite-time are analyzed using the Lyapunov function method. The validity and practicability of the proposed method are verified by a numerical example.
KW - Fractional-order sliding-mode guidance law (FOSMGL)
KW - lag compensation
KW - miniature munition
KW - piecewise trajectory planning
UR - http://www.scopus.com/inward/record.url?scp=85161493741&partnerID=8YFLogxK
U2 - 10.1109/TAES.2023.3281310
DO - 10.1109/TAES.2023.3281310
M3 - Article
AN - SCOPUS:85161493741
SN - 0018-9251
VL - 59
SP - 6782
EP - 6797
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 5
ER -