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基于滑模干扰观测器的垂直攻击末制导律研究
引用本文:朱凯,齐乃明.基于滑模干扰观测器的垂直攻击末制导律研究[J].兵工学报,2011,32(12):1462-1467.
作者姓名:朱凯  齐乃明
作者单位:(哈尔滨工业大学 航天学院, 黑龙江 哈尔滨 150001)
摘    要:针对导弹高精度、垂直打击地面目标的任务要求,将滑模干扰观测器和比例导引律相结合,提出了一种满足多约束条件的鲁棒性末制导方法.综合考虑落点、落角等约束条件,给出了纵向平面和侧向平面的比例导引系数的选取原则.为了弥补比例导引的不足,提高制导系统的鲁棒性,基于滑模干扰观测器对不确定性进行了估计,确保了系统对导引指令的精确跟踪...

关 键 词:飞行器控制、导航技术  导弹  末制导  比例导引  垂直攻击  滑模干扰观测器

Research on Vertical Impact Terminal Guidance Law Based on Sliding Mode Disturbance Observer
ZHU Kai , QI Nai-ming.Research on Vertical Impact Terminal Guidance Law Based on Sliding Mode Disturbance Observer[J].Acta Armamentarii,2011,32(12):1462-1467.
Authors:ZHU Kai  QI Nai-ming
Affiliation:(School of Astronautics, Harbin Institute of Technology, Harbin 150001, Heilongjiang, China)
Abstract:The problem of terminal precision guidance for missiles with vertical attack angle constraint is considered.A sliding mode disturbance observer and enhanced adaptive proportional guidance law are applied to improve the robustness.Considering the constraints of target location and attack angle,the guidance parameters selections in longitudinal and lateral planes are analyzed.The uncertainties of the dynamics are estimated by using a second-order sliding mode disturbance observer,and then compensated to ensure high accuracy in the realization of guidance commands.Simulation results demonstrate the robustness and accuracy of the proposed approach.Compared with the conventional adaptive proportional guidance approach,the guidance precision of proposed approach is obviously improved in the present of aerodynamic dispersions.
Keywords:control and navigation technology of aerocraft  missile  terminal guidance  proportional guidance  vertical attack  sliding mode disturbance observer
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