首页 | 官方网站   微博 | 高级检索  
     

自主学习干扰观测器驱动的重复使用运载器再入段滑模控制
引用本文:陈佳晔,穆荣军,白瑜亮,张新,崔乃刚.自主学习干扰观测器驱动的重复使用运载器再入段滑模控制[J].宇航学报,2019,40(6):694-702.
作者姓名:陈佳晔  穆荣军  白瑜亮  张新  崔乃刚
作者单位:哈尔滨工业大学航天工程系,哈尔滨 150001
摘    要:针对重复使用运载器(RLV)再入段的姿态控制问题,设计一种具有自主学习干扰观测器(SLDO)的滑模控制器。基于奇异摄动理论及时标分离原则,将RLV的姿态动力学方程划分为外环和内环子系统。根据RLV再入段模型不确定性和外部干扰均随时间变化、不可忽略且无法预知边界等特点,结合2型模糊神经结构、误差反馈学习架构以及滑模控制(SMC)理论,提出一种新型在线自主学习干扰观测器。设计基于SLDO驱动的多元超螺旋滑模控制器,完成对再入段姿态的跟踪。最后,针对6自由度RLV模型进行了仿真分析,仿真结果证明了控制方法的有效性以及鲁棒性。

关 键 词:重复使用运载器(RLV)  自主学习干扰观测器(SLDO)  滑模控制(SMC)  再入段姿态跟踪  
收稿时间:2018-07-09

Sliding Mode Control in Reentry Phase for a Reusable Launch Vehicle Driven by a Self Learning Disturbance Observer
CHEN Jia ye,MU Rong jun,BAI Yu liang,ZHANG Xin,CUI Nai gang.Sliding Mode Control in Reentry Phase for a Reusable Launch Vehicle Driven by a Self Learning Disturbance Observer[J].Journal of Astronautics,2019,40(6):694-702.
Authors:CHEN Jia ye  MU Rong jun  BAI Yu liang  ZHANG Xin  CUI Nai gang
Affiliation:Department of Aerospace Engineering, Harbin Institute of Technology, Harbin 150001, China
Abstract: A sliding mode controller based on self-learning disturbance observer (SLDO) is designed for a reusable launch vehicle (RLV). According to the singular perturbation theory, a RLV dynamic model is divided into the outer-loop and inner-loop subsystems. Since the model uncertainties and the disturbances vary with time and have unknown boundaries, combining with the type-2 neuro-fuzzy structure, feedback-error learning scheme and sliding mode control (SMC) theory, a novel online SLDO is presented. The multivariable supertwisting sliding mode controller driven by a SLDO is designed to track the re-entry trajectory precisely and convergent rapidly. Finally, by the simulation and analysis of the 6-degree-of-freedom model of RLV in the reentry phase, the effectiveness and the robustness of the integrated control scheme are verified.
Keywords:Reusable launch vehicle (RLV)  Self-learning disturbance observer (SLDO)  Sliding mode control (SMC)  Reentry attitude track  
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司    京ICP备09084417号-23

京公网安备 11010802026262号