基于一致性理论的多飞行器自主编队控制及协同制导方法研究

With the rapid development of the aerospace technology and the increasing complexity of the battlefield environment, the single-flight-vehicle combat have been unable to meet the requirements in future air combat missions. In order to enhance the performance of the defense system and improve the attack precision, the multiple flight vehicles cooperative interception has become a major defensive tactic in the military field. With the background of cooperative interception by multiple flight vehicles, this project mainly research the formation control and cooperative guidance problems. To meet the practical requirements of cooperative interception missions, studies will be carried out on the finite-time autonomous formation control method considering the detection configuration, the finite-time parameter adaptive cooperative guidance method based on leader-follower strategy, and the cooperative estimation method of maneuvering target state based on the consistent theory, which provides reasonable solutions to the special problems brought by multiple flight vehicles cooperative control. By combining the multi-agent finite time consensus theory with the multiple flight vehicles cooperative control system, the better control performance with faster dynamics and stronger robustness can be achieved. This project lays a theoretical foundation for the development of key technologies and the expansion of application fields through the in-depth study of the multiple flight vehicles cooperative control system.

随着航空航天技术的不断提高，战场环境也日益复杂，单一飞行器已经无法满足未来空战的要求。为了增强防御系统性能，提高打击精度，采用多飞行器进行协同拦截成为国内外军事领域关注的防御战术。本项目以多飞行器协同拦截来袭机动目标为研究背景，针对中末制导过程中的编队飞行控制和协同制导等问题展开研究，面向协同拦截任务的实际要求，开展考虑探测构型的有限时间自主编队控制方法、基于领导-跟随策略的有限时间参数自适应协同制导方法及基于一致性理论的机动目标状态协同估计方法等研究工作，为多飞行器协同控制带来的特殊问题给出合理的解决方案。通过将多智能体系统有限时间一致性理论与多飞行器协同控制系统有机结合，实现速度更快、鲁棒性更好的控制效果。本项目对多飞行器协同控制理论体系进行系统研究，可以为关键技术的发展和应用领域的拓展奠定理论基础。

随着航空航天技术的不断提高，战场环境也日益复杂，单一飞行器已经无法满足未来空战的要求。为了增强防御系统性能，提高打击精度，采用多飞行器进行协同拦截成为国内外军事领域关注的防御战术。本项目以多飞行器协同拦截来袭机动目标为研究背景，针对中末制导过程中的编队飞行控制和协同制导等问题展开研究，面向协同拦截任务的实际要求，开展了考虑探测构型的有限时间自主编队控制方法、基于领导-跟随策略的有限时间参数自适应协同制导方法及基于一致性理论的机动目标状态协同估计方法等研究工作，为多飞行器协同控制带来的特殊问题给出合理的解决方案。通过将多智能体系统有限时间一致性理论与多飞行器协同控制系统有机结合，实现了速度更快、鲁棒性更好的控制效果。本项目对多飞行器协同控制理论体系进行了系统研究，可以为关键技术的发展和应用领域的拓展奠定理论基础。