TY - JOUR
T1 - Appointed-time prescribed performance attitude tracking control via double performance functions
AU - Yin, Zeyang
AU - Suleman, Afzal
AU - Luo, Jianjun
AU - Wei, Caisheng
N1 - Publisher Copyright:
© 2019 Elsevier Masson SAS
PY - 2019/10
Y1 - 2019/10
N2 - This work investigates the attitude tracking control problem of spacecraft under strong external disturbances and parameter uncertainties. A novel appointed-time stable control scheme is proposed with guaranteed transient and steady-state performance. First, an appointed-time reachable performance function (ARPF) is presented, and its reach time can be arbitrarily selected by the users. Then, a double-ARPFs strategy is introduced, that is, by imposing two ARPFs on the attitude and the system output, respectively, all system states will be appointed-time stable. Furthermore, a robust controller with implementable structure is proposed to guarantee the performance functions under strong external disturbances and parameter uncertainties. And the attitude tracking errors as well as the angular velocity errors are proved to be appointed-time stable. Last, three groups of simulations are organized to verify the effectiveness, robustness and appointed-time stability of the proposed control scheme.
AB - This work investigates the attitude tracking control problem of spacecraft under strong external disturbances and parameter uncertainties. A novel appointed-time stable control scheme is proposed with guaranteed transient and steady-state performance. First, an appointed-time reachable performance function (ARPF) is presented, and its reach time can be arbitrarily selected by the users. Then, a double-ARPFs strategy is introduced, that is, by imposing two ARPFs on the attitude and the system output, respectively, all system states will be appointed-time stable. Furthermore, a robust controller with implementable structure is proposed to guarantee the performance functions under strong external disturbances and parameter uncertainties. And the attitude tracking errors as well as the angular velocity errors are proved to be appointed-time stable. Last, three groups of simulations are organized to verify the effectiveness, robustness and appointed-time stability of the proposed control scheme.
KW - Appointed-time stability
KW - Attitude control
KW - Finite-time control
KW - Low-complexity control
KW - Prescribed performance control
UR - http://www.scopus.com/inward/record.url?scp=85070880440&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2019.105337
DO - 10.1016/j.ast.2019.105337
M3 - 文章
AN - SCOPUS:85070880440
SN - 1270-9638
VL - 93
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 105337
ER -