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1. 北京理工大学 宇航学院, 北京 100081
2. 航天科工智能运筹与信息安全研究院(武汉)有限公司, 湖北 武汉 430040
Received:11 March 2022,
Published Online:07 August 2023,
Published:30 July 2023
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Yu HAN, Tao SONG, Duo ZHENG, et al. Unmanned Aerial Vehicle Cluster Cooperative Guidance Technology Based on Conflict Trigger Mechanism[J]. Acta Armamentarii, 2023, 44(7): 1881-1895.
Yu HAN, Tao SONG, Duo ZHENG, et al. Unmanned Aerial Vehicle Cluster Cooperative Guidance Technology Based on Conflict Trigger Mechanism[J]. Acta Armamentarii, 2023, 44(7): 1881-1895. DOI: 10.12382/bgxb.2022.0152.
协同打击是提升飞行器集群整体作战效能的重要模式。针对密集飞行器集群协同打击目标过程中存在的相互碰撞或彼此干扰问题
建立典型的多目标协同打击的任务场景模型
揭示飞行器集群协同运动过程中的机动规律;基于效用函数最优理论研究避免碰撞的飞行器集群协调最优机动策略
保证飞行器之间避免碰撞。考虑飞行器集群协同制导中的时间/空间同步到达约束
采用基于时间管控的多约束协同制导策略
同时满足到达时间和脱靶量要求;引入基于冲突触发的协同避碰机制
提出兼顾避碰和协同打击的协同调整策略
求得满足避免碰撞与时空同步的协同制导方法。仿真结果表明
新提出的考虑避碰约束的飞行器集群协同制导方法能够保证飞行器间的安全距离约束
具有较强的协同时间管控能力和较高的制导精度
且仅需较少迭代计算
降低了对机载处理器的要求
为飞行器集群协同打击中的避碰问题提供了一种解决方法
具有较强的工程应用价值。
Cooperative strike is an important mode to improve the overall combat effectiveness of aircraft clusters. To address the problem of mutual collision or interference in the process of cooperative attack on targets by dense aircraft clusters
a typical mission scenario model of multi-target cooperative attack is established
and the maneuver law in the process of cooperative movement of aircraft cluster is revealed. Then
based on the optimal theory of utility function
the coordinated optimal maneuver strategy of aircraft cluster to avoid collision is studied
ensuring collision avoidance between aircrafts. Considering the time/space synchronous arrival constraint in aircraft cluster cooperative guidance
a multi-constraint cooperative guidance strategy based on time control is adopted
which meets the requirements of arrival time and miss distance at the same time. On this basis
a cooperative collision avoidance mechanism based on conflict triggering is introduced
and a cooperative adjustment strategy that considers collision avoidance and cooperative attack is proposed. And a cooperative guidance method satisfying collision avoidance and spatio-temporal synchronization is obtained. The simulation results show that the proposed aircraft cluster cooperative guidance method considering collision avoidance constraints ensures safe distance constraints between aircrafts and has strong aircraft cluster cooperative time control ability and high guidance accuracy. It requires less iterative calculation
reduces the requirements for airborne processors
and provides a solution to the collision avoidance problem in aircraft cluster cooperative attack. This method has strong engineering application value.
闵海波 , 刘源 , 王仕成 , 等 . 多个体协调控制问题综述 [J ] . 自动化学报 , 2012 , 38 ( 10 ): 1557 - 1570 .
MIN H B , LIU Y , WANG S C , et al . An overview on coordination control problem of multi-agent system [J ] . Acta Automatica Sinica , 2012 , 38 ( 10 ): 1557 - 1570 . (in Chinese) DOI: 10.3724/SP.J.1004.2012.01557 http://doi.org/10.3724/SP.J.1004.2012.01557 http://www.aas.net.cn/cn/article/doi/10.3724/SP.J.1004.2012.01557 http://www.aas.net.cn/cn/article/doi/10.3724/SP.J.1004.2012.01557
MCLAIN T W , BEARD R W . Coordination variables,coordination functions,and cooperative timing missions [J ] . Journal of Guidance Control & Dynamics , 2005 , 28 ( 1 ): 150 - 161 .
JEON I , LEE J , TAHK M . Impact-time-control guidance law for anti-ship missiles [J ] . IEEE Transactions on Control Systems Technology , 2006 , 14 ( 2 ): 260 - 266 . DOI: 10.1109/TCST.2005.863655 http://doi.org/10.1109/TCST.2005.863655 https://ieeexplore.ieee.org/document/1597196/ https://ieeexplore.ieee.org/document/1597196/
张友安 , 马国欣 , 王兴平 . 多导弹时间协同制导:一种领弹-被领弹策略 [J ] . 航空学报 , 2009 , 30 ( 6 ): 1109 - 1118 . 首先,假设各枚导弹的速度为相同常值,领弹采用经典比例导引(PNG),被领弹采用经典比例导引和机动控制相结合的方式,推导出采用领弹-被领弹策略的多导弹时间协同控制设计模型,该模型实际上描述的是一个非线性的弹目相对运动状态跟踪控制系统。在此系统中,领弹的弹目距离与导弹前置角作为两个参考状态量,被领弹的弹目距离与导弹前置角作为两个待控制的状态量。针对这一弹目相对运动状态跟踪控制系统,采用时标分离的方法设计了期望的慢子系统和快子系统。对这两个子系统分别进行动态逆控制设计,得到了被领弹的机动控制指令。该机动控制指令用于调整被领弹相对目标的运动状态,来逼近领弹相对目标的运动状态,这就保证了所有的导弹能够同时攻击目标。然后,通过为每枚被领弹引入一个与其速度相同的虚拟领弹,将上述方法推广到各枚导弹速度可为不同常值的情况。仿真结果验证了本文方法的有效性。
ZHANG Y A , MA G X , WANG X P . Time-cooperative guidance for multi-missiles:a leader-follower strategy [J ] . Acta Aeronautica et Astronautica Sinica , 2009 , 30 ( 6 ): 1109 - 1118 . (in Chinese)
赵世钰 , 周锐 . 基于协调变量的多导弹协同制导 [J ] . 航空学报 , 2008 , 29 ( 6 ): 1605 - 1611 .
ZHAO S Y , ZHOU R . Multi-missile cooperative guidance using coordination variables [J ] . Acta Aeronautica et Astronautica Sinica , 2008 , 29 ( 6 ): 1605 - 1611 . (in Chinese)
王晓芳 , 郑艺裕 , 林海 . 多导弹协同作战制导律研究 [J ] . 弹道学报 , 2014 , 26 ( 1 ): 61 - 66 . 为了增强多枚反舰导弹协同作战时的突防和打击能力,提出了一种由弹目距离协同制导律和视线角速度收敛制导律两部分组成的多导弹协同制导律。综合多枚导弹的弹目距离信息,设计了期望弹目距离。基于比例导引律建立了导弹目标相对运动非线性模型,采用时标分离原理将其分为快变子系统和慢变子系统,然后采用动态逆系统理论将2个子系统反馈线性化,基于线性系统理论设计了能够实现多弹弹目距离趋于期望弹目距离的制导律。为了保证各导弹顺利地协同攻击目标,在飞行末段,采用有限时间控制理论设计了在弹目距离逐渐缩小的过程中视线角速度在有限时间内快速收敛到零的制导律。仿真结果表明:采用该协同制导律能够使多枚导弹以期望的弹目距离同步接近目标,最后几乎同时命中目标,有效地实现了弹目距离和攻击时间的协同。
WANG X F , ZHENG Y Y , LIN H . Research on guidance law for cooperative attack of multiple mis-siles [J ] . Journal of Ballistics , 2014 , 26 ( 1 ): 61 - 66 . (in Chinese)
赵启伦 , 陈建 , 董希旺 , 等 . 拦截高超声速目标的异类导弹协同制导律 [J ] . 航空学报 , 2016 , 37 ( 3 ): 936 - 948 . DOI: 10.7527/S1000-6893.2015.0235 http://doi.org/10.7527/S1000-6893.2015.0235 对于多导弹协同拦截高超声速目标的问题,设计了一种具有领弹-从弹拓扑结构的异类导弹协同制导律:配备有高性能导引头的领弹采用改进比例导引法拦截目标;未配备导引头的从弹利用通信手段,采用二阶一致性跟踪算法,对领弹进行跟踪。两类导弹同时命中目标,形成"多对一"的拦截态势。异构型的制导策略可以降低对导引设备的需求,具备较理想的作战效费比。领弹与从弹的弹道均源于改进比例导引法,具有较理想的弹道特性。给出了协同制导律在固定拓扑与切换拓扑下成立的充分条件。算例仿真验证了所提出的制导律能够实现对高超声速目标的协同拦截,具有良好的可行性。
ZHAO Q L , CHEN J , DONG X W , et al . Cooperative guidance law for hetero-geneous missiles intercepting hypersonic weapon [J ] . Acta Aeronautica et Astronautica Sinica , 2016 , 37 ( 3 ): 936 - 948 . (in Chinese)
马国欣 , 张友安 . 多导弹时间协同分布式导引律设计 [J ] . 控制与决策 , 2014 , 29 ( 5 ): 843 - 847 .
MA G X , ZHANG Y A . Time-cooperative distribut-ed guidance law design for multi-missiles [J ] . Control & Decision , 2014 , 29 ( 5 ): 843 - 847 . (in Chinese)
王天宁 , 张世隆 , 葛航 . 考虑目标观测度的领从式协同制导研究 [J ] . 飞行力学 , 2021 , 39 ( 5 ): 56 - 62 .
WANG T N , ZHANG S L , GE H . Research of leader-follower cooperative guidance considering the target observability [J ] . Flight Dynamics , 2021 , 39 ( 5 ): 56 - 62 . (in Chinese)
TABASSO C , CICHELLA V . Multiple leader-follower coor-dination for cooperative missions [C ] //Proceedings of AIAA Scitech 2021 Forum, Multi-Agent Control and Coordination I, Virtual Event. Reston, VA , US : AIAA , 2021 : 1766 .
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) DOI: 10.3969/j.issn.1000-1093.2021.08.008 http://doi.org/10.3969/j.issn.1000-1093.2021.08.008 A reinforcement learning-based cooperative guidance law utlitizing a deep deterministic policy gradient descent neural network is proposed to achieve the cooperative attack of multiple missiles against a target and improve the attack effectiveness. The estimation equation of time-to-go based on the linear engagement dynamics is revised to improve the estimation accuracy of time-to-go, which is no longer restricted by the assumption of small angle. The time-to-go error of each missile is regarded as the coordination variable. The time-to-go error and range-to-go of each missile are used as the observables of the reinforcement learning algorithm. The reward function is constructed by using miss distance and time-to-go error, and then a reinforcement learning agent is generated by offline training. In the process of closed-loop guidance, the reinforcement learning agent generates guidance commands in real time, by that simultaneous attack can be achieved. Simulated results verify that the proposed reinforcement learning guidance law can achieve simultaneous attack on the target. Compared with the traditional cooperative guidance law, the reinforcement learning cooperative guidance law can be used to obtain smaller miss distances and smaller attack time errors.
KROZEL J , PETERS M E , HUNTER G . Conflict detection and resolution for future air transportation management [R ] . Washington, D.C. , US : NASA , 1997 .
TOMLIN C , PAPPAS G J , SASTRY S . Conflict resolution for air traffic management: a study in multiagent hybrid systems [J ] . IEEE Transactions on Automatic Control AC , 1998 , 43 ( 4 ): 509 - 52 . DOI: 10.1109/9.664154 http://doi.org/10.1109/9.664154 http://ieeexplore.ieee.org/document/664154/ http://ieeexplore.ieee.org/document/664154/
CHEN W F , CHEN J Y , SHAO Z J , et al . Three-Dimensional aircraft conflict resolution based on smoothing methods [J ] . Journal of Guidance,Control,and Dynamics , 2016 , 39 ( 7 ): 1481 - 1490 . DOI: 10.2514/1.G001726 http://doi.org/10.2514/1.G001726 https://arc.aiaa.org/doi/10.2514/1.G001726 https://arc.aiaa.org/doi/10.2514/1.G001726
OMER J . A space-discretized mixed-integer linear model for air-conflict resolution with speed and heading maneuvers [J ] . Computers & Operations Research , 2015 ,58 (Jun.) : 75 - 86 .
HILL J C , ARCHIBALD J K , STIRLING W C , et al . A multi-agent system architecture for distributed air traffic control [C ] //Proceedings of AIAA Guidance, Navigation, and Control Conference and Exhibit, Distributed /Decentralized Air Traffic Control. San Francisco, CA , US : AIAA , 2005 : 6049 .
ARCHIBALD J K , et al . A satisficing approach to aircraft conflict resolution [J ] . IEEE Transactions on Systems,Man,and Cybernetics,Part C(Applications and Reviews) , 2008 , 38 ( 4 ): 510 - 521 .
BREITENMOSER A , MARTINOLI A . On combining multi-robot coverage and reciprocal collision avoidance [M ] .Tokyo, Japan:Springer , 2016 : 49 - 64 .
ALONSO-AYUSO A , ESCUDERO L F , MARTIN-CAMPO F J . Collision avoidance in air traffic management:a mixed-integer linear optimization approach [J ] . IEEE Transactions on Intelligent Transportation Systems , 2011 , 12 ( 1 ): 47 - 57 . DOI: 10.1109/TITS.2010.2061971 http://doi.org/10.1109/TITS.2010.2061971 http://ieeexplore.ieee.org/document/5551203/ http://ieeexplore.ieee.org/document/5551203/
ALONSO-AYUSO A , ESCUDERO L F , MARTIN-CAMPO F J . On modeling the air traffic control coordination in the collision avoidance problem by mixed integer linear optimization [J ] . Annals of Operations Research , 2014 , 222 : 89 - 105 . DOI: 10.1007/s10479-013-1347-y http://doi.org/10.1007/s10479-013-1347-y http://link.springer.com/10.1007/s10479-013-1347-y http://link.springer.com/10.1007/s10479-013-1347-y
杨健 . 无人机集群系统空域冲突消解方法研究 [D ] . 长沙 : 国防科学技术大学 , 2016 : 101 - 123 .
YANG J . Study on the airspace conflict resolution problem of unmanned aerial vehicle swarm systems [D ] . Changsha : National University of Defense Technology , 2016 : 101 - 123 . (in Chinese)
赵毓 , 郭继峰 , 郑红星 , 等 . 基于强化学习的多无人机避碰计算制导方法 [J ] . 导航定位与授时 , 2021 , 8 ( 1 ): 31 - 40 .
ZHAO Y , GUO J F , ZHENG H X , et al . A reinforcement learning based computational guidance approach for UAVs collision avoidance [J ] . Navigation Positioning and Timing , 2021 , 8 ( 1 ): 31 - 40 . (in Chinese)
CHOI D , CHHABRA A , KIM D . Collision avoidance of unmanned aerial vehicles using fuzzy inference system-aided enhanced potential field [C ] //Proceedings of AIAA Scitch 2022 Forum, Multi-Agent Control and Coordination. San Diego, CA , US : AIAA , 2022 : 272 .
TONY L A , GHOSE D , CHAKRAVARTHY A . Unmanned aerial vehicle mid-air collision detection and resolution using avoidance maps [J ] . Journal of Aerospace Information Systems , 2021 , 18 ( 8 ): 506 - 529 . DOI: 10.2514/1.I010900 http://doi.org/10.2514/1.I010900 https://arc.aiaa.org/doi/10.2514/1.I010900 https://arc.aiaa.org/doi/10.2514/1.I010900
DUBINS L E . On plane curves with curvature [J ] . Pacific Journal of Mathematics , 1961 , 11 ( 2 ): 471 - 481 . DOI: 10.2140/pjm http://doi.org/10.2140/pjm http://msp.org/pjm/ http://msp.org/pjm/
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