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引入战斗机人工势场的概念,建立针对主从编队引导控制的模型。在分析势、势场力的基础上,构建战斗机编队的队形势以及队形力函数。建立编队控制模型,编队队形的结构与队形参考点有关,参考点的数量和位置由队形和队形控制方式决定,主从编队控制以长机为队形参考点。建立了基于队形力的主从编队控制模型,并应用于实际领航者之中。仿真表明飞行误差收敛速度快,僚机能够稳定跟踪领航者的飞行轨迹,并保持较小的跟踪误差(20～40m)。在密集编队控制中,仍需改进控制器和优化参数;在稀疏队形和分散队形中,完全可以满足控制需要。
The concept of artificial potential field of fighter aircraft was introduced and a model of guidance control for main and subordinate formations was established. Based on the analysis of potential and potential force, the team formation and formation force function of fighter formation are built. The formation control model is established. The structure of formation formation is related to the formation reference point. The number and position of reference points are determined by the formation and formation control methods. The main and subordinate formations control are long formation reference points. Established a master-slave formation control model based on formation force and applied it to the actual pilot. The simulation shows that the flight error converges fast, the wingman can stably track the leader’s flight path and keep the tracking error (20 ~ 40m) less. In dense formation control, the controller and optimization parameters still need to be improved. In sparse formation and dispersed formation, the control needs to be fully met.