TY - JOUR
T1 - Hybrid Disturbance Observer-Based Anti-Disturbance Composite Control with Applications to Mars Landing Mission
AU - Xu, Jianwei
AU - Yu, Xiang
AU - Qiao, Jianzhong
N1 - Publisher Copyright:
© 2013 IEEE.
PY - 2021/5
Y1 - 2021/5
N2 - In this paper, a hybrid anti-disturbance composite control scheme is presented to address the problem subject to systems remarkably affected by external disturbances and discrete dynamics of actuators. By explicitly considering the hybrid feature resulting from discrete actuation signals acted on a continuous system, the hybrid disturbance observer is designed to estimate the effect of external disturbance. Meanwhile, {H_{infty }} technique is used to mitigate the effect of continuous command executing error caused by discontinuous operation, which cannot be modeled in priori. Within the proposed composite control scheme, the combination of the disturbance estimation information and the {H_{infty }} technique enables the entire hybrid system precisely performing. The stability of the whole continuous-discrete control system is analyzed. Finally, based on the Mars lander dynamics, comparative simulation studies illustrate that the developed control scheme can preserve a satisfactory level of performance, even in the presence of external disturbances and actuator quantization errors.
AB - In this paper, a hybrid anti-disturbance composite control scheme is presented to address the problem subject to systems remarkably affected by external disturbances and discrete dynamics of actuators. By explicitly considering the hybrid feature resulting from discrete actuation signals acted on a continuous system, the hybrid disturbance observer is designed to estimate the effect of external disturbance. Meanwhile, {H_{infty }} technique is used to mitigate the effect of continuous command executing error caused by discontinuous operation, which cannot be modeled in priori. Within the proposed composite control scheme, the combination of the disturbance estimation information and the {H_{infty }} technique enables the entire hybrid system precisely performing. The stability of the whole continuous-discrete control system is analyzed. Finally, based on the Mars lander dynamics, comparative simulation studies illustrate that the developed control scheme can preserve a satisfactory level of performance, even in the presence of external disturbances and actuator quantization errors.
KW - Anti-disturbance composite control
KW - Mars landing powered descent phase
KW - hybrid disturbance observer
KW - multiple sources of disturbances
UR - https://www.scopus.com/pages/publications/85086984651
U2 - 10.1109/TSMC.2019.2917528
DO - 10.1109/TSMC.2019.2917528
M3 - 文章
AN - SCOPUS:85086984651
SN - 2168-2216
VL - 51
SP - 2885
EP - 2893
JO - IEEE Transactions on Systems, Man, and Cybernetics: Systems
JF - IEEE Transactions on Systems, Man, and Cybernetics: Systems
IS - 5
M1 - 8730351
ER -