输入约束反演滑模控制器的再入飞行器轮廓跟踪控制

R. Tang, Biao Luo, Yuxin Liao
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引用次数: 0

摘要

针对高超声速飞行器再入滑翔相位制导问题,提出了一种基于输入约束反步滑模控制器(BSMC)的轮廓跟踪控制方法。首先,将滑翔相位的多路径约束转化为阻力-加速度-速度(D-V)剖面中的再入通道;以二次函数的形式设计标准轮廓,并通过智能算法对函数系数进行优化。基于拖曳加速度和速度的二阶微分模型,利用辅助系统设计了一个输入约束的BSMC,以获取车辆纵向运动所需的控制命令。最后,通过再入滑翔阶段的数值仿真验证了该控制方案的跟踪性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Profile Tracking Control of Reentry Vehicle With Input-constrained Backstepping Sliding Mode Controller
In view of the reentry glide phase guidance problem of hypersonic vehicles, this paper proposes a profile tracking control method based on input-constrained backstepping sliding mode controller (BSMC). First, the multiple path constraints of gliding phase are transformed into the reentry corridor in the drag acceleration-velocity (D-V) profile. A standard profile is designed in the form of a quadratic function, and the function coefficients are optimized by the intelligent algorithm. Based on the second-order differential model of drag acceleration and velocity, an input-constrained BSMC is designed by using the auxiliary system to obtain the control commands required for the longitudinal motion of vehicle. Finally, the tracking performance of the control scheme is verified by numerical simulation of reentry gliding phase.
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