系统工程与电子技术

• 制导、导航与控制 • 上一篇    下一篇

SO(3)上的内蕴滑模观测器设计与应用

刘超, 唐胜景, 郭杰, 王喻林   

  1. 北京理工大学宇航学院飞行动力学与控制教育部重点实验室, 北京 100081
  • 出版日期:2017-02-25 发布日期:2010-01-03

Design and application of intrinsic sliding-mode observer on SO(3)

LIU Chao, TANG Shengjing, GUO Jie, WANG Yulin   

  1. Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081
  • Online:2017-02-25 Published:2010-01-03

摘要:

基于李群的动力学系统建模方法不依赖局部坐标和浸入空间的特性,因而常被用于描述一般力学系统。针对一类基于李群SO(3)描述的力学系统,考虑了实际姿态位形可测但角速度不可测的情况,利用SO(3)上曲率张量、Levi-Civita联络及测地线等内蕴信息,设计了SO(3)上的Super-Twisting内蕴滑模观测器,对实际姿态位形和旋转角速度进行观测,并在其切空间内分析了所设计观测器的收敛性能。最后将所设计的观测器应用在四旋翼平台并进行仿真,仿真结果表明,所设计的观测器具有较好的观测效果和较强的鲁棒性。

Abstract:

Modelling with Lie group in mechanical systems is widely used in numerous fields, because the method does not depend on local coordinates and peculiarities of immersive space. Considering the situation that configuration manifold is measurable but the angular speed is not measurable, a Super-Twisting intrinsic observer for a class of system built on SO(3) is designed with the intrinsic geometric information, such as Levi-Civita connection, curvature tensor and geodesic. The observer is used to obtain the angular speed and configuration manifold for the system. Observer convergence speciality is provided in the tangent space of SO(3). Then the observer is applied on a quadrotor testbed, the simulation result shows the perfect performance and robustness of the designed observer.