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张源 , 张冉 , 李惠峰 . 复杂禁飞区无动力滑翔飞行器路径-轨迹双层规划 [J ] . 宇航学报 , 2022 , 43 ( 5 ): 615 - 627 .

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朱金冬 , 张方齐 , 赵彤 . 任务规划系统机动模型与航线设计 [J ] . 航空工程进展 , 2022 , 13 ( 4 ): 73 - 82 .

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王磊 , 徐超 , 李淼 , 等 . 多飞行器协同任务分配的改进粒子群优化算法 [J ] . 兵工学报 , 2023 , 44 ( 8 ): 2224 - 2232 . DOI: 10.12382/bgxb.2022.0968 http://doi.org/10.12382/bgxb.2022.0968 为提升多飞行器编队执行任务的效率和性能,提出一种用于多飞行器协同任务分配的改进粒子群优化算法。考虑飞行器任务能力约束,飞行器执行任务时付出的威胁代价、航程代价以及完成任务的收益,从而构造问题的数学模型。将粒子的位置属性编码为一组任务分配向量,从任务分配向量可解码出对应的任务分配解,实现粒子群优化算法解的离散化。为解决粒子群优化算法容易陷入局部收敛的缺点,提出一种跳出局部收敛的策略。该策略基于模拟退火算法,生成新粒子,以一定概率决定是否保留新粒子,并将跳出局部收敛的策略应用到传统粒子群优化算法中,建立可用于多飞行器协同任务分配的改进粒子群优化算法。数字仿真实验结果表明,与现有算法相比,所提算法能显著提高多飞行器任务分配的收益和效率。

WANG L , XU C , LI M , et al . Improved particle swarm optimization algorithm for multi-aircraft collaborative task assignment [J ] . Acta Armamentarii , 2023 , 44 ( 8 ): 2224 - 2232 . (in Chinese) DOI: 10.12382/bgxb.2022.0968 http://doi.org/10.12382/bgxb.2022.0968 An improved particle swarm optimization (PSO) algorithm for multi-aircraft cooperative task assignment is proposed. The corresponding mathematical model is developed by considering the constraints of the aircraft’s capability, the threat cost, the range cost, and the benefits obtained by completing the tasks. The position attribute of particles is encoded as a set of task assignment vectors, from which we can decode the task assignment solution such that the PSO solution is discretized. In order to solve the problem that the PSO algorithm can easily fall into local convergence, a strategy of jumping out of the local convergence is proposed. Based on the simulated annealing algorithm, this strategy first generates new particles, and then decides whether to retain the new particles with a certain probability. Finally, this jumping-out strategy is applied to the conventional PSO algorithm so as to establish an improved one that can be used for multi-aircraft cooperative task assignment. The digital simulation results verify the effectiveness of the proposed algorithm.

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魏昀鹏 , 都延丽 , 王文凯 , 等 . 无动力滑翔飞行器时间协同预测校正鲁棒制导 [J ] . 宇航学报 , 2024 , 45 ( 3 ): 421 - 432 .

WEI Y P , DU Y L , WANG W K , et al . Time-cooperative Predictor corrector Robust Guidance for unpowered vehicles [J ] . Journal of Astronautics , 2024 , 45 ( 3 ): 421 - 432 . (in Chinese)

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姜鹏 , 郭栋 , 韩亮 , 等 . 多飞行器再入段时间协同弹道规划方法 [J ] . 航空学报 , 2020 , 41 ( 增刊1 ): 723776 .

JIANG P , GUO D , HAN L , et al . Cooperative ballistic planning method for multi-craft re-entry time [J ] . Acta Aeronautica et Astronautica Sinica , 2020 , 41 ( S1 ): 723776 . (in Chinese) DOI: 10.7527/S1000-6893.2019.23776 http://doi.org/10.7527/S1000-6893.2019.23776 This paper presents a trajectory optimization method for the cooperative reentry of multiple hypersonic glide vehicles. First, the nominal longitudinal trajectory is planned to satisfy the path and terminal constraints. Second, the trajectory tracking law is used to track the nominal longitudinal trajectory. Meanwhile, a multi-layer bounded corridor for heading error considering the initial lateral state is proposed to control the lateral maneuver, so as to meet the requirement of arrival time and the terminal constraints. Then the trajectory planning with arrival time constraints for a single vehicle is implemented. On this basis, the arrival time distribution and the flight capability are analyzed, and the analysis and the calculation methods for the minimum and the maximum arrival time are given. For the multiple hypersonic glide vehicle cooperative reentry scenario, the cooperative flight time decision-making is completed. Finally, numerical results show that the trajectory optimization method achieves a good performance on the arrival time and the terminal constraints, which indicates that the proposed method can realize the cooperative reentry of multiple hypersonic glide vehicle. The results in dispersed cases indicate that the trajectory optimization method has good calculation accuracy and robustness.

乔浩 , 毛瑞 , 白凤科 , 等 . 带时间约束的双参数再入轨迹设计方法 [J ] . 弹箭与制导学报 , 2021 , 41 ( 3 ) : 57 - 61 . DOI: 10.15892/j.cnki.djzdxb.2021.03.013 http://doi.org/10.15892/j.cnki.djzdxb.2021.03.013 为实现再入飞行时间可控,扩展现有再入飞行器的应用场景,提高对时间敏感目标的打击能力,以双参数牛顿迭代法为基础,提出一种改进的阻力加速度剖面设计方法,通过设置双参数校正点,能够同时对轨迹长度与总飞行时间进行设计。在给定的轨迹长度与总飞行时间约束下,该方法能够快速完成参考阻力加速度剖面的迭代,生成满足各项约束的参考轨迹。通过仿真分析获得了再入总飞行时间的调节规律,为多再入飞行器的协同攻击问题提供依据。

QIAO H , MAO R , BAI F K , et al . Two-parameter reentry trajectory design method with time constraints [J ] . Journal of Projectiles,Rockets,Missiles and Guidance , 2021 , 41 ( 3 ): 57 - 61 . (in Chinese)

池海红 , 周明鑫 . 融合强化学习和进化算法的无动力滑翔航迹规划 [J ] . 控制理论与应用 , 2022 , 39 ( 5 ): 847 - 856 .

CHI H H , ZHOU M X . Trajectory planning for unpowered vehicle combined with reinforcement learning and evolutionary algorithms [J ] . Control Theory & Applications , 2022 , 39 ( 5 ): 847 - 856 . (in Chinese)

张晚晴 , 余文斌 , 李静琳 , 等 . 基于纵程解析解的飞行器智能横程机动再入协同制导 [J ] . 兵工学报 , 2021 , 42 ( 7 ): 1400 - 1411 .

ZHANG W Q , XU W B , LI J L , et al . Cooperative reentry guidance for intelligent lateral maneuver of hypersonic vehicle based on downrange analytical solution [J ] . Acta Armamentarii , 2021 , 42 ( 7 ): 1400 - 1411 . (in Chinese) DOI: 10.3969/j.issn.1000-1093.2021.07.007 http://doi.org/10.3969/j.issn.1000-1093.2021.07.007 A cooperative guidance law based on deep Q-learning network (DQN) algorithm for lateral maneuver of hypersonic vehicles is proposed to meet the requirement of cooperative saturation attack. The longitudinal and lateral guidance laws are deigned. The longitudinal lift-to-drag ratio is calculated to obtain the modulus of bank angle based on the high-precision longitudinal analytical solution. The lateral bank reversal logic is abstracted as a Markov decision process (MDP), and the reinforcement learning method can be used. A lateral intelligent maneuver decision-making device based on DQN algorithm is designed. The intelligent agent can be generated by offline training according to the mission requirements, and is called online to generate the sign of bank angle. Simulated results show that the proposed guidance law can autonomously generate bank angle reversals on-line, strictly meets the requirements of flight time constraints and energy management, and has high guidance accuracy and good mission adaptability. Compared with the coordinative reentry guidance law based on three-dimensional analytical solutions, the proposed guidance law is used to fully achieve the lateral maneuverability of vehicle and make it have higher penetration potential.

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王少平 , 董受全 , 隋先辉 , 等 . 助推滑翔无动力滑翔导弹发展趋势及作战使用研究 [J ] . 战术导弹技术 , 2020 ( 1 ): 9 - 14 .

WANG S P , DONG S Q , SUI X H , et al . Research on development and operational application of boost-glide unpowered missile [J ] . Tactical Missile Technology , 2020 ( 1 ): 9 - 14 . (in Chinese)

LI Z , WANG Y D , ZHENG W . Adaptively tracking hypersonic gliding vehicles [J ] . Aerospace Science and Technology , 2024 , 147 : 109035 .

ZHOU H Y , WANG X G , LI X , et al . Synergistic planning for hypersonic vehicles with an analytic hybrid algorithm [J ] . IEEE Transactions on Aerospace and Electronic Systems , 2025 , 61 ( 1 ): 223 - 232 .

张磊 , 罗迎 , 张群 . 雷达组网系统对抗有源干扰方法综述 [J ] . 信息对抗技术 , 2023 , 2 ( 6 ): 1 - 16 .

ZHANG L , LU Y , ZHANG Q . Summary of counteracting active jamming method of radar networking system [J ] . Information Countermeasure Technology , 2023 , 2 ( 6 ): 1 - 16 . (in Chinese)

韩晓斐 , 何华锋 , 何耀民 , 等 . 主被动异构弹载雷达组网抑制假目标干扰方法 [J ] . 兵工学报 , 2022 , 43 ( 12 ): 3142 - 3150 .

HAN X F , HE H F , HE Y M , et al . A method against false-target jamming based on active/passive isomerism missile-borne radar network [J ] . Acta Armamentarii , 2022 , 43 ( 12 ) : 3142 - 3150 . (in Chinese) DOI: 10.12382/bgxb.2021.0716 http://doi.org/10.12382/bgxb.2021.0716 Single missile-borne radars are unable to effectively cope with false target jamming in a complex battlefield environment due to a single angle of view, a lack of information, and low anti-jamming efficacy. A method against false-target jamming is thus proposed based on an active/passive missile-borne radar network. This method considers the position error of the missile-borne radar. When the track first begins, angle information is used to identify the measurements of active and passive radar seekers, and some false targets are eliminated. The track initiation of passive missile borne radar is assisted by successfully correlated measurements of the active missile borne radar. Then, the targets are tracked separately by the active and passive missile-borne radars. During track correlation, tracks are associated to identify and eliminate the remaining false targets. Simulation results show that the proposed method can effectively suppress the false-target jamming based on deceptive distance while ensuring high real target discrimination probability.

张俊 , 胡生亮 , 杨庆 , 等 . 浮空式角反射体RCS统计特征及识别模型研究 [J ] . 系统工程与电子技术 , 2019 , 41 ( 4 ): 780 - 786 .

ZHANG J , HU S L , YANG Q , et al . RCS statistical features and recognition model of air-floating corner reflector [J ] . Systems Engineering and Electronics , 2019 , 41 ( 4 ): 780 - 786 . (in Chinese)

宋瑞 , 朱勇 , 徐广通 , 等 . 基于序列凸优化的高超声速飞行器协同再入轨迹规划 [J ] . 战术导弹技术 , 2020 ( 6 ): 7 - 16 .

SONG R , ZHU Y , XU G T , et al . Cooperative reentry trajectory planning of hypersonic vehicle based on sequential convex programming [J ] . Tactical Missile Technology , 2020 ( 6 ): 7 - 16 . (in Chinese)