TY - JOUR
T1 - Three-Dimensional Fixed-Time Cooperative Guidance Law with Impact Angle Constraint and Prespecified Impact Time
AU - Lin, Mu
AU - Ding, Xiangjun
AU - Wang, Chunyan
AU - Liang, Li
AU - Wang, Jianan
N1 - Publisher Copyright:
© 2013 IEEE.
PY - 2021
Y1 - 2021
N2 - In this paper, by utilizing fixed-time control technique and a leader-follower control scheme, a three-dimensional (3-D) cooperative guidance law is developed to tackle impact angle constrained simultaneous arrival problem. Firstly, in the line-of-sight (LOS) direction, guidance command for the leader is put forward to make impact time error converge to zero in fixed time such that the leader is capable of reaching the target at prespecified impact time. Then, guidance command for each follower is designed based on information from adjacent interceptors to guarantee each follower's impact time achieves consensus with that of the leader. Secondly, in the azimuth direction and elevation direction of the LOS, guidance commands are put forward to nullify the LOS angular rates within fixed time. Then, the interceptors are able to reach the target with desired impact angles. Meanwhile, the cooperative guidance law's fixed-time convergence is rigorously proved by Lyapunov stability theory. Finally, simulations are given to illustrate the effectiveness of the theoretical results.
AB - In this paper, by utilizing fixed-time control technique and a leader-follower control scheme, a three-dimensional (3-D) cooperative guidance law is developed to tackle impact angle constrained simultaneous arrival problem. Firstly, in the line-of-sight (LOS) direction, guidance command for the leader is put forward to make impact time error converge to zero in fixed time such that the leader is capable of reaching the target at prespecified impact time. Then, guidance command for each follower is designed based on information from adjacent interceptors to guarantee each follower's impact time achieves consensus with that of the leader. Secondly, in the azimuth direction and elevation direction of the LOS, guidance commands are put forward to nullify the LOS angular rates within fixed time. Then, the interceptors are able to reach the target with desired impact angles. Meanwhile, the cooperative guidance law's fixed-time convergence is rigorously proved by Lyapunov stability theory. Finally, simulations are given to illustrate the effectiveness of the theoretical results.
KW - 3-D cooperative guidance
KW - Fixed-time control
KW - impact angle constraint
KW - leader-follower control scheme
KW - prespecified impact time
UR - http://www.scopus.com/inward/record.url?scp=85101473893&partnerID=8YFLogxK
U2 - 10.1109/ACCESS.2021.3057428
DO - 10.1109/ACCESS.2021.3057428
M3 - Article
AN - SCOPUS:85101473893
SN - 2169-3536
VL - 9
SP - 29755
EP - 29763
JO - IEEE Access
JF - IEEE Access
M1 - 9348900
ER -