TY - GEN
T1 - Three-dimensional Multi-missile Cooperative Guidance Law with Time and Space Constraints
AU - Meng, Jian
AU - Yang, Zhen
AU - Huang, Jichuan
AU - Piao, Haiyin
AU - Zhao, Yiyang
AU - Zhou, Deyun
N1 - Publisher Copyright:
© 2022 ICROS.
PY - 2022
Y1 - 2022
N2 - This study focuses on the problem of multiple air-to-air missiles coordinated intercepting maneuvering targets in three-dimensional (3-D) space. A fixed time cooperative interception law with attack time and line-of-sight (LOS) angle limitations is proposed. Firstly, we extended the commonly used two-dimensional (2-D) space guidance model to 3-D space, and constructs a 3-D missile-target relative motion model. Secondly, the missile guidance model is decoupled to along and perpendicular to the LOS, and in the LOS direction, a cooperative guiding law based on fixed-time consistency theory is intended to guarantee that all missiles strikes the target at the same moment. Moreover, in the LOS normal direction, an adaptive approach rule is created, and the LOS angle of each missile is regulated to reaching to a given value in a defined time. According to the proposed fixed time fast non-singular terminal sliding mode surface, and spatial coordination is accomplished. In addition, based on Lyapunov stability theory, a detailed fixed time stability analysis is given. In the end, simulation is used to verify the feasibility and efficacy of the guideline law.
AB - This study focuses on the problem of multiple air-to-air missiles coordinated intercepting maneuvering targets in three-dimensional (3-D) space. A fixed time cooperative interception law with attack time and line-of-sight (LOS) angle limitations is proposed. Firstly, we extended the commonly used two-dimensional (2-D) space guidance model to 3-D space, and constructs a 3-D missile-target relative motion model. Secondly, the missile guidance model is decoupled to along and perpendicular to the LOS, and in the LOS direction, a cooperative guiding law based on fixed-time consistency theory is intended to guarantee that all missiles strikes the target at the same moment. Moreover, in the LOS normal direction, an adaptive approach rule is created, and the LOS angle of each missile is regulated to reaching to a given value in a defined time. According to the proposed fixed time fast non-singular terminal sliding mode surface, and spatial coordination is accomplished. In addition, based on Lyapunov stability theory, a detailed fixed time stability analysis is given. In the end, simulation is used to verify the feasibility and efficacy of the guideline law.
KW - 3-D
KW - Adaptive approach law
KW - Cooperative guidance
KW - Fast nonsingular terminal sliding mode
KW - Fixed-time consistency
KW - LOS angle constraints
UR - http://www.scopus.com/inward/record.url?scp=85146583254&partnerID=8YFLogxK
U2 - 10.23919/ICCAS55662.2022.10003825
DO - 10.23919/ICCAS55662.2022.10003825
M3 - 会议稿件
AN - SCOPUS:85146583254
T3 - International Conference on Control, Automation and Systems
SP - 931
EP - 937
BT - 2022 22nd International Conference on Control, Automation and Systems, ICCAS 2022
PB - IEEE Computer Society
T2 - 22nd International Conference on Control, Automation and Systems, ICCAS 2022
Y2 - 27 November 2022 through 1 December 2022
ER -