为满足高速飞行器编队对协同误差的快速收敛性能需求，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，建立二阶系统模型及编队误差动力学模型。然后，设计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，继而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文本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 rapid convergence performance requirements of high-speed aircraft, a finite-time inverse optimization composite control strategy is proposed. First, simplify the dynamic model of the high-speed aircraft, establish a second-order system model and a formation error dynamic model. Then, a finite-time convergent sliding mode control method is designed to enhance the convergence speed of cooperative errors in high-speed aircraft formations, meeting the real-time requirements of cooperative control during rapid maneuvers. On the basis of finite-time convergence, an inverse optimization composite control method is further proposed to improve the cooperative control performance of the system, aiming to satisfy specified optimal performance metrics. Finally, the effectiveness and feasibility of the text-based inverse optimization composite control method based on limited time were verified through simulation experiments.