ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Time-constrained multi-missile cooperative guidance law
Received date: 2024-04-25
Revised date: 2024-04-26
Accepted date: 2024-05-23
Online published: 2024-05-31
Supported by
Natural Science Foundation of China(61827901)
This article addresses the problem of time-coordinated strike against weakly maneuvering targets. The implicit cooperative guidance problem based on the constant velocity motion model and the explicit cooperative guidance problem based on the velocity time-varying model are studied to enhance the breakthrough and destruction capabilities of anti-tank missiles against high-value targets. Firstly, based on the assumption of missile motion at a constant velocity, the idea of predictive correction and the optimal error dynamics theory are employed. Time-constrained bias terms are added to the proportional navigation guidance law, and a time-constrained guidance law is derived based on optimal error dynamics. An implicit time-coordinated guidance law scenarios depending weakly on communication is then proposed. To address the issue that inaccurate time prediction affects the performance of implicit cooperation caused by variable speed missile strikes, a neural network-based explicit time-coordinated guidance method is further proposed. This method adopts the predictive correction guidance framework, and designs the predictor by using transfer learning integrated neural networks according to the characteristics of proportional navigation guidance law to accurately predict the remaining flight time. Consistency dynamics with specified time convergence is proposed to coordinate the lengths of missile trajectories in the distributed communication architecture, ensuring that multiple missiles simultaneously hit the target. Simulation results show that the proposed implicit time-coordinated guidance method can ensure that multiple missiles simultaneously hit the target accurately, and the neural network-based explicit time-coordinated guidance method proposed can ensure coordinated strikes against multiple missiles under variable speed conditions.
Zichao LIU , Jiang WANG , Peng WANG , Defu LIN , Zhichuan HE . Time-constrained multi-missile cooperative guidance law[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2024 , 45(S1) : 730607 -730607 . DOI: 10.7527/S1000-6893.2024.30607
1 | 王笑梦, 杨吾帆. “轻矛” 与“坚盾” 的较量[N]. 解放军报, 2022-05-20(9). |
WANG X M, YANG W F. “Light spear” versus “strong shield”[N]. People’s Liberation Army Daily, 2022-05-20(9) (in Chinese). | |
2 | 王岐朋, 王韩, 李嘉诚. 俄乌冲突中的“流量” 武器及战术[J]. 轻兵器, 2022(6): 44-46. |
WANG Q P, WANG H, LI J C. “Flow” weapons and tactics in the conflict between Russia and Ukraine[J]. Small Arms, 2022(6): 44-46 (in Chinese). | |
3 | 程刚. “陆战王者” 的克星: 反坦克导弹[J]. 军事文摘, 2021(18): 16-19. |
CHENG G. Anti-tank missile: the Nemesis of “king of land warfare”[J]. Military Digest, 2021(18): 16-19 (in Chinese). | |
4 | 玉琮. 美国陆军新一代重型远程反坦克导弹选型[J]. 坦克装甲车辆, 2021(17): 47-53. |
YU C. Selection of new generation heavy-duty long-range anti-tank missile of US army[J]. Tank & Armoured Vehicle, 2021(17): 47-53 (in Chinese). | |
5 | 赵曙光, 孙娟芬, 杜佳原, 等. 反坦克导弹软件系统指标体系研究[J]. 航空兵器, 2021, 28(6): 104-110. |
ZHAO S G, SUN J F, DU J Y, et al. Research on software system technical index of the anti-tank guided missile[J]. Aero Weaponry, 2021, 28(6): 104-110 (in Chinese). | |
6 | 姜增良, 原树兴, 邵云峰, 等. 直瞄反坦克导弹火力转移射击问题研究[J]. 火力与指挥控制, 2021, 46(10): 160-163. |
JIANG Z L, YUAN S X, SHAO Y F, et al. Research on fire shift shooting problem of direct-fire anti-tank missile[J]. Fire Control & Command Control, 2021, 46(10): 160-163 (in Chinese). | |
7 | JEON I S, LEE J I, TAHK M J. Impact-time-control guidance law for anti-ship missiles[J]. IEEE Transactions on Control Systems Technology, 2006, 14(2): 260-266. |
8 | KIM T H, LEE C H, TAHK M J, et al. Biased PNG law for impact-time control[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2013, 56(4): 205-214. |
9 | JEON I S, LEE J I, TAHK M J. Impact-time-control guidance with generalized proportional navigation based on nonlinear formulation[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(8): 1885-1890. |
10 | WANG Y J, DONG S, OU L L, et al. Cooperative control of multi-missile systems[J]. IET Control Theory & Applications, 2015, 9(3): 441-446. |
11 | LEE S, CHO N, KIM Y. Impact-time-control guidance strategy with a composite structure considering the seeker’s field-of-view constraint[J]. Journal of Guidance, Control, and Dynamics, 2020, 43(8): 1566-1574. |
12 | JEON I S, LEE J I, TAHK M J. Homing guidance law for cooperative attack of multiple missiles[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(1): 275-280. |
13 | LI K, WANG J N, LEE C H, et al. Distributed cooperative guidance for multivehicle simultaneous arrival without numerical singularities[J]. Journal of Guidance, Control, and Dynamics, 2020, 43(7): 1365-1373. |
14 | 阮聪, 温求遒, 孙国鑫. 考虑速度时变的多约束攻击时间控制制导律[J]. 战术导弹技术, 2020(3): 59-65. |
RUAN C, WEN Q Q, SUN G X. Multi-constraint impact time control guidance law under time-varying velocity[J]. Tactical Missile Technology, 2020(3): 59-65 (in Chinese). | |
15 | DONG W, WANG C Y, WANG J N, et al. Varying-gain proportional navigation guidance for precise impact time control[J]. Journal of Guidance, Control, and Dynamics, 2022, 46(3): 535-552. |
16 | GUO Y H, LI X, ZHANG H J, et al. Data-driven method for impact time control based on proportional navigation guidance[J]. Journal of Guidance, Control, and Dynamics, 2020, 43(5): 955-966. |
17 | SUN G X, WEN Q Q, XU Z Q, et al. Impact time control using biased proportional navigation for missiles with varying velocity[J]. Chinese Journal of Aeronautics, 2020, 33(3): 956-964. |
18 | 方科, 张庆振, 倪昆, 等. 高超声速飞行器时间协同再入制导[J]. 航空学报, 2018, 39(5): 321958. |
FANG K, ZHANG Q Z, NI K, et al. Time-coordinated reentry guidance law for hypersonic vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(5): 321958 (in Chinese). | |
19 | LIU Z C, WANG J, HE S M, et al. Learning prediction-correction guidance for impact time control[J]. Aerospace Science and Technology, 2021, 119: 107187. |
20 | 陈中原, 韦文书, 陈万春. 基于强化学习的多发导弹协同攻击智能制导律[J]. 兵工学报, 2021, 42(8): 1638-1647. |
CHEN Z Y, WEI W S, CHEN W C. Reinforcement learning-based intelligent guidance law for cooperative attack of multiple missiles[J]. Acta Armamentarii, 2021, 42(8): 1638-1647 (in Chinese). | |
21 | YUCELEN T, KAN Z, PASILIAO E. Finite-time cooperative engagement[J]. IEEE Transactions on Automatic Control, 2019, 64(8): 3521-3526. |
22 | HE S M, LEE C H. Optimality of error dynamics in missile guidance problems[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(7): 1624-1633. |
23 | WANG C Y, DONG W, WANG J N, et al. Guidance law design with fixed-time convergent error dynamics[J]. Journal of Guidance, Control, and Dynamics, 2021, 44(7): 1389-1398. |
24 | YOSINSKI J, CLUNE J, BENGIO Y, et al. How transferable are features in deep neural networks?[J]. Advances in Neural Information Processing Systems, 2014, 4(January): 3320-3328. |
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