高速飞行器编队有限时间逆优化复合控制OA
Finite-time inverse optimization composite control of high-speed aircraft formation
为满足高速飞行器编队的协同误差应快速收敛这一性能需求,提出一种基于有限时间的逆优化复合控制策略.首先,对高速飞行器动力学模型进行简化,建立二阶系统模型和编队误差动力学模型.然后,设计了一种有限时间收敛的滑模控制方法,用于提升高速飞行器编队协同误差的收敛速度,以满足高速飞行器在快速机动过程中对协同控制的实时性要求;为了在有限时间收敛的基础上进一步提升系统的协同控制性能,提出了一种逆优化复合控制方法,旨在满足指定的最优性能指标.最终,通过仿真实验验证了所提出的基于有限时间的逆优化复合控制方法的有效性和可行性.
To meet the performance requirements of rapid convergence of cooperative errors for high-speed aircraft formation,a finite-time inverse optimization composite control strategy is proposed.Firstly,the dynamic model of the high-speed aircraft is simplified,and a second-order system model along with a formation error dynamic model is es-tablished.Then,a sliding mode control method with finite-time convergence is designed to enhance the convergence speed of cooperative errors in high-speed aircraft formation,thereby meeting the real-time requirements of cooperative control during rapid maneuvers.To further enhance the cooperative performance on the basis of finite-time conver-gence,an inverse optimization composite control method is proposed to satisfy specified optimal performance metrics.Finally,simulation experiments verify the effectiveness and feasibility of the proposed finite-time inverse optimization composite control method.
郭晋利;陈谋
南京航空航天大学 自动化学院,南京 211100南京航空航天大学 自动化学院,南京 211100
航空航天
高速飞行器编队协同控制有限时间控制逆优化控制滑模控制
high-speed aircraft formationcooperative controlfinite-time controlinverse optimization controlslid-ing mode control
《航空学报》 2026 (z1)
57-66,10
国家自然科学基金(U23B2036,62533012)空基信息感知与融合全国重点实验室基金(ZH2024-0058)江苏省科技计划专项资金港澳台科技合作计划(BZ2023057) National Natural Science Foundation of China(U23B2036,62533012)National Key Laboratory Fund of Air-Based Information Perception and Fusion(ZH2024-0058)Special Fund for Science and Technology Planning Projects of Jiangsu Province:Hong Kong,Macao and Taiwan Science and Technology Cooperation Project(BZ2023057)
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