TY - JOUR
T1 - Three-dimensional piecewise cooperative guidance with smooth switching topology
AU - Chen, Shiwei
AU - Wang, Wei
AU - Fan, Junfang
N1 - Publisher Copyright:
© 2024 Elsevier Masson SAS
PY - 2024/7
Y1 - 2024/7
N2 - To investigate the issue of large-scale multi-missile cooperative attacks on a same target, this paper presents a three-dimensional piecewise cooperative guidance law based on smooth switching topology, realizing time consensus and impact angle constraints. Firstly, to implement the piecewise cooperative guidance law design, we establish the attack surface of the arc profile according to the expected LOS angle and the communication switching point, and obtain the virtual impact point (VIP). Secondly, a switching function is designed to ensure the smooth transition of the communication topology, mitigating the chattering issue in existing communication topology switching, while a time consensus protocol control input is implemented to facilitate the time cooperative attack of the missile in the LOS direction. Meanwhile, a fixed-time terminal sliding mode guidance law is established to guarantee the satisfaction of the impact angle constraint at the VIP. Additionally, an adaptive three-dimensional proportional navigation guidance (PNG) law is designed to guarantee zero miss distance at the real impact point (RIP). Finally, simulations involving four missiles attacking stationary targets simultaneously validate the effectiveness and superiority of the piecewise cooperative guidance law.
AB - To investigate the issue of large-scale multi-missile cooperative attacks on a same target, this paper presents a three-dimensional piecewise cooperative guidance law based on smooth switching topology, realizing time consensus and impact angle constraints. Firstly, to implement the piecewise cooperative guidance law design, we establish the attack surface of the arc profile according to the expected LOS angle and the communication switching point, and obtain the virtual impact point (VIP). Secondly, a switching function is designed to ensure the smooth transition of the communication topology, mitigating the chattering issue in existing communication topology switching, while a time consensus protocol control input is implemented to facilitate the time cooperative attack of the missile in the LOS direction. Meanwhile, a fixed-time terminal sliding mode guidance law is established to guarantee the satisfaction of the impact angle constraint at the VIP. Additionally, an adaptive three-dimensional proportional navigation guidance (PNG) law is designed to guarantee zero miss distance at the real impact point (RIP). Finally, simulations involving four missiles attacking stationary targets simultaneously validate the effectiveness and superiority of the piecewise cooperative guidance law.
KW - Communication topology switching
KW - Fixed-time terminal sliding mode guidance law
KW - Impact angle constraint
KW - Piecewise cooperative guidance law
KW - Time consensus protocol control
UR - https://www.scopus.com/pages/publications/85192853710
U2 - 10.1016/j.ast.2024.109181
DO - 10.1016/j.ast.2024.109181
M3 - Article
AN - SCOPUS:85192853710
SN - 1270-9638
VL - 150
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 109181
ER -