TY - JOUR
T1 - 面向弹道导弹防御的快速最优拦截弹道规划
AU - Li, Yaxuan
AU - Wang, Yan
AU - Liu, Xinfu
N1 - Publisher Copyright:
© 2024 Chinese Society of Astronautics. All rights reserved.
PY - 2024/12
Y1 - 2024/12
N2 - A rapid optimal intercept trajectory planning method based on neural network is proposed for solving the intercept trajectory planning problem of ballistic missile defense. Firstly,the optimal intercept trajectory cluster is generated by optimizing the trajectory of the powered phase. Then,the optimal intercept point and intercept trajectory with respect to the maximum intercept velocity are determined based on the optimal intercept trajectory cluster. To improve the efficiency,the neural networks are used to establish the mapping relationships between the intercept point and the intercept velocity,intercept time,and trajectory parameters. For the trajectory optimization problem of the powered phase,a trajectory optimization algorithm based on nonlinearity-kept convexification is proposed. This paper integrate the nonlinearity of dynamics by using the Taylor formula,properly preserve the nonlinearity by defining new variables and introducing new constraints,and then linearize an obtained control-affine system to get linear dynamics. This method effectively improves the convergence of the algorithm,and the convergence issue caused by directly linearizing dynamics can be avoided. Simulation results demonstrate that the proposed method has good reliability and real-time performance.
AB - A rapid optimal intercept trajectory planning method based on neural network is proposed for solving the intercept trajectory planning problem of ballistic missile defense. Firstly,the optimal intercept trajectory cluster is generated by optimizing the trajectory of the powered phase. Then,the optimal intercept point and intercept trajectory with respect to the maximum intercept velocity are determined based on the optimal intercept trajectory cluster. To improve the efficiency,the neural networks are used to establish the mapping relationships between the intercept point and the intercept velocity,intercept time,and trajectory parameters. For the trajectory optimization problem of the powered phase,a trajectory optimization algorithm based on nonlinearity-kept convexification is proposed. This paper integrate the nonlinearity of dynamics by using the Taylor formula,properly preserve the nonlinearity by defining new variables and introducing new constraints,and then linearize an obtained control-affine system to get linear dynamics. This method effectively improves the convergence of the algorithm,and the convergence issue caused by directly linearizing dynamics can be avoided. Simulation results demonstrate that the proposed method has good reliability and real-time performance.
KW - Intercept trajectory planning
KW - Neural network
KW - Optimal intercept point
KW - Successive convex optimization
KW - Trajectory optimization
UR - http://www.scopus.com/inward/record.url?scp=85214505241&partnerID=8YFLogxK
U2 - 10.3873/j.issn.1000-1328.2024.12.007
DO - 10.3873/j.issn.1000-1328.2024.12.007
M3 - 文章
AN - SCOPUS:85214505241
SN - 1000-1328
VL - 45
SP - 1931
EP - 1943
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 12
ER -