纵向静不稳定火箭弹过载控制自动驾驶仪设计

摘要

开展静不稳定火箭弹设计有利于提高火箭弹的机动和射程能力，从火箭弹低成本的要求出发对静不稳定火箭弹自动驾驶仪进行了设计，提出过载反馈自动驾驶仪形式及参数设计方法，对控制系统设备动态特性对系统性能的影响进行分析，结果表明该方案可有效指导火箭弹的设计。%The static unstable design conduces to enhancing the maneuver capability and range of artillery rockets. To lower the cost, an autopilot is designed for longitudinal static unstable artillery rockets in this paper. Additionally, the form and parameter design method of the overload feedback autopilot are proposed, which is followed by an analysis about the effect of equipment’s dynamic characteristics of control system on system performance. The results can serve as an effective reference for artillery rocket design.