倾斜转弯飞行器分布式编队制导控制一体化设计  

Integrated guidance and control design for distributed formation of BTT aircrafts

作　　者：陈昶荣 刘珊 许鑫 Chen Changrong;Liu Shan;Xu Xin(Beijing Electro-mechanical Engineering Institute,Beijing 100074,China;Science and Technology on Complex System Control and Intelligent Agent Cooperation Laboratory,Beijing 100074,China)

机构地区：[1]北京机电工程研究所,北京100074 [2]复杂系统控制与智能协同技术重点实验室,北京100074

出　　处：《战术导弹技术》2024年第5期139-150,共12页Tactical Missile Technology

摘　　要：针对高速飞行情况下倾斜转弯(Bank To Turn,BTT)飞行器编队控制问题,基于一种制导控制一体化(Integrated Guidance and Control,IGC)理论提出一种分布式编队系统建模与控制器设计方法。通过坐标变换,将双积分系统模型与BTT飞行器动力学模型相结合,得到了IGC模型;在反演控制框架下,采用一致性理论与神经网络自适应滑模变结构理论设计了编队控制器;进行严格的理论分析并证明了闭环系统的稳定性和收敛特性;在高速情况下进行了六自由度数学仿真,仿真结果表明了IGC设计方法的有效性,以及较传统设计方法的优越性。Distributed formation control problem of bank-to-turn(BTT)aircraft at high-speed condition is considered,and a modeling and controller design method based on the integrated guidance and control(IGC)theory is proposed.The IGC model is obtained by combining the double integrating system model with the BTT aircraft dynamics model through transforming coordinate.The formation controller is designed based on consistent algorithm and neural network adaptive sliding mode variable structure theory in the structure of the backstepping control.Meanwhile,the stability and convergence property of the closed-loop system is analyzed and proven strictly.The six degree of freedom numerical simulation is carried out at high-speed condition.The simulation results show that the IGC design method is effective and superior to the traditional design method.

关 键 词：分布式编队 制导控制一体化 倾斜转弯 反演控制 一致性理论 神经网络 滑模变结构 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]