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欠驱动再入飞行器的抗饱和姿态控制器设计

李宪强 周军

火力与指挥控制2016,Vol.41Issue(12):15-19,5.
火力与指挥控制2016,Vol.41Issue(12):15-19,5.

欠驱动再入飞行器的抗饱和姿态控制器设计

Attitude Tracking of the Under-actuated Reentry Vehicle with Actuator Saturation

李宪强 1周军2

作者信息

  • 1. 北京空间技术研制试验中心,北京 100094
  • 2. 西北工业大学精确制导与控制研究所,西安 710072
  • 折叠

摘要

Abstract

In this paper,an attitude tracking controller for the under-actuated reentry vehicle with only two actuators is designed in the presence of actuator saturation and disturbance. During design of the controller,the attitude kinematics and dynamics model of under-actuated reentry vehicle is firstly divided into a slow-loop subsystem and a under-actuated fast-loop subsystem. And then a super-twisting sliding mode controller and an adaptive hierarchical sliding mode controller are designed separately for the slow-loop subsystem and fast-loop subsystem. Finally,the validation of the method is verified through simulation.

关键词

欠驱动/再入飞行器/饱和/分层滑模

Key words

under-actuated/reentry vehicle/saturation/hierarchical sliding mode

分类

军事科技

引用本文复制引用

李宪强,周军..欠驱动再入飞行器的抗饱和姿态控制器设计[J].火力与指挥控制,2016,41(12):15-19,5.

基金项目

国家自然科学基金资助项目(61403028) (61403028)

火力与指挥控制

OA北大核心CSCDCSTPCD

1002-0640

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