TY - JOUR
T1 - Fixed-time anti-saturation grouped cooperative guidance law with state estimations of multiple maneuvering targets
AU - Ma, Xiang
AU - Dai, Keren
AU - Zou, Yao
AU - Yu, Hang
AU - Zhang, He
AU - Wang, Xiaofeng
N1 - Publisher Copyright:
© 2023 The Franklin Institute
PY - 2023/5
Y1 - 2023/5
N2 - The problem of a grouped multiple missiles cooperative attack on multiple high maneuvering targets with a limited driving force is achieved by an anti-saturation fixed-time grouped cooperative guidance (FxTCG) law based on a sliding mode fixed-time disturbance observer (SM-FxTDO) in this study. First, the state estimation of each high maneuvering target within a fixed time is achieved by designing a sliding mode fixed-time disturbance observer. Second, the group cooperative guidance law is designed by using fixed-time theory, which can ensure the group consensus of multiple missiles strike times within a fixed time under the condition of input saturation. Then, the fixed time stability of the multi-missiles system is proven by using the bi-limit homogeneous theory and the Lyapunov function. Finally, the simulation results show the superiority of the designed observer and cooperative guidance law. The proposed observer can more effectively and accurately estimate the state of the high maneuvering target than the ESO. The proposed cooperative guidance law expands the number of attack targets and makes each group of multiple missiles attack the corresponding high maneuvering target under the conditions of an input saturation within a fixed time compared to the single-target cooperative law.
AB - The problem of a grouped multiple missiles cooperative attack on multiple high maneuvering targets with a limited driving force is achieved by an anti-saturation fixed-time grouped cooperative guidance (FxTCG) law based on a sliding mode fixed-time disturbance observer (SM-FxTDO) in this study. First, the state estimation of each high maneuvering target within a fixed time is achieved by designing a sliding mode fixed-time disturbance observer. Second, the group cooperative guidance law is designed by using fixed-time theory, which can ensure the group consensus of multiple missiles strike times within a fixed time under the condition of input saturation. Then, the fixed time stability of the multi-missiles system is proven by using the bi-limit homogeneous theory and the Lyapunov function. Finally, the simulation results show the superiority of the designed observer and cooperative guidance law. The proposed observer can more effectively and accurately estimate the state of the high maneuvering target than the ESO. The proposed cooperative guidance law expands the number of attack targets and makes each group of multiple missiles attack the corresponding high maneuvering target under the conditions of an input saturation within a fixed time compared to the single-target cooperative law.
UR - http://www.scopus.com/inward/record.url?scp=85152481080&partnerID=8YFLogxK
U2 - 10.1016/j.jfranklin.2023.02.031
DO - 10.1016/j.jfranklin.2023.02.031
M3 - Article
AN - SCOPUS:85152481080
SN - 0016-0032
VL - 360
SP - 5524
EP - 5547
JO - Journal of the Franklin Institute
JF - Journal of the Franklin Institute
IS - 8
ER -