TY - GEN
T1 - Closed Loop Guidance with Ballistic Inclination Constraint and the Curve Planning Based Energy Management
AU - Guo, Dong
AU - Gong, Min
AU - Gao, Feng
AU - Dong, Xiwang
AU - Ren, Zhang
N1 - Publisher Copyright:
© 2022, The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
PY - 2022
Y1 - 2022
N2 - In this paper, an improved closed loop guidance method for solid ballistic missile is presented. Firstly, the dynamics model of the rocket is established in the launch inertial coordinate system. Then the conversion relation between the launch coordinate system and the launch inertial coordinate system is illustrated. Secondly, based on the traditional closed loop guidance scheme, an improved closed loop guidance method with the ballistic inclination constraint of the reentry point is presented, which by introducing the reentry point velocity information. Then, to achieve the management of the remaining energy of the solid rocket, a curve planning based energy management scheme is adopted. Combined with the proposed closed loop guidance scheme, the guidance commands which satisfying the complex constraint can be generated in real time. Finally, multiple scenarios under nominal and disturbance conditions are simulated to verify the proposed closed loop guidance with energy management scheme. Results indicate that the proposed method has good attack accuracy and task adaptability.
AB - In this paper, an improved closed loop guidance method for solid ballistic missile is presented. Firstly, the dynamics model of the rocket is established in the launch inertial coordinate system. Then the conversion relation between the launch coordinate system and the launch inertial coordinate system is illustrated. Secondly, based on the traditional closed loop guidance scheme, an improved closed loop guidance method with the ballistic inclination constraint of the reentry point is presented, which by introducing the reentry point velocity information. Then, to achieve the management of the remaining energy of the solid rocket, a curve planning based energy management scheme is adopted. Combined with the proposed closed loop guidance scheme, the guidance commands which satisfying the complex constraint can be generated in real time. Finally, multiple scenarios under nominal and disturbance conditions are simulated to verify the proposed closed loop guidance with energy management scheme. Results indicate that the proposed method has good attack accuracy and task adaptability.
KW - Ballistic inclination constraint
KW - Closed loop guidance
KW - Disturbance conditions
KW - Energy management
KW - Reentry point
UR - https://www.scopus.com/pages/publications/85120604477
U2 - 10.1007/978-981-15-8155-7_429
DO - 10.1007/978-981-15-8155-7_429
M3 - 会议稿件
AN - SCOPUS:85120604477
SN - 9789811581540
T3 - Lecture Notes in Electrical Engineering
SP - 5203
EP - 5214
BT - Advances in Guidance, Navigation and Control - Proceedings of 2020 International Conference on Guidance, Navigation and Control, ICGNC 2020
A2 - Yan, Liang
A2 - Duan, Haibin
A2 - Yu, Xiang
PB - Springer Science and Business Media Deutschland GmbH
T2 - International Conference on Guidance, Navigation and Control, ICGNC 2020
Y2 - 23 October 2020 through 25 October 2020
ER -