动态杀伤飞行器侧装窗口定位算法及姿态控制器设计

Lu Cang-hai, Cai Yuan-li, Zhi Qiang
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引用次数: 2

摘要

为了解决高速飞行引起的气动热问题,KKV采用了侧窗探测技术。提出了一种新的侧窗定位算法,根据视距角度调整KKV姿态角,实现对目标的稳定精确跟踪。采用时尺度分离方法实现侧窗算法。采用脉冲方式激活姿态推力器,采用脉宽脉频调制控制姿态推力器发射。PWPF调制是一种为开关推力器提供伪线性操作的控制方法。与经典的bang-bang控制器相比,PWPF调制器具有几个优点,例如接近线性操作,精度高,减少推进剂消耗。本文采用一种带有阈值限制的改进型PWPF调制器,以减少推进器点火次数和燃料消耗,但可能以控制精度为代价。通过计算机仿真对控制方案进行了验证。实验结果证明了该方案的可行性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Side-Mounted Window Orientation Algorithm and Attitude Controller Design for Kinetic Kill Vehicle
Side-window detection technology is adopted by the kinetic kill vehicle (KKV) to solve the problem of aerodynamic heat induced by the high speed. A new side-window orientation algorithm is proposed to adjust the KKV attitude angles according to the line-of-sight (LOS) angles to achieve stable and accurate tracking of the target. The time-scale separation methodology is adopted to implement the side window algorithm. The attitude thrusters are activated in pulse mode, and the pulse-width pulse-frequency (PWPF) modulation is adopted to control the thrusters firing. PWPF modulation is a control method that provides pseudo-linear operation for an on-off thruster. PWPF modulator holds several advantages over classical bang-bang controllers such as close to linear operation, high accuracy, and reduced propellant consumption. A modified PWPF modulator with threshold limitation is adopted in this paper to reduce the number of thruster firings and fuel consumption at a possible cost of control accuracy. The control scheme is verified using computer simulation. The results have been proven the potential of this scheme.
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