Adaptive Integral-type Sliding Mode Control for Spacecraft Attitude Maneuvering Under Actuator Stuck Failures

Author:

HU Qinglei,ZHANG Youmin,HUO Xing,XIAO Bing

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference41 articles.

1. Rotational maneuvers of nonlinear uncertain spacecraft;Singh;IEEE Transactions on Aerospace Electronic and Systems,1988

2. Dynamics and control of flexible multi-body systems Part II: simulation code and parametric studies with nonlinear control;Nagata;Acta Astronautica,2001

3. Stiffening control of a class of nonlinear affine systems;Karray;IEEE Transactions on Aerospace Electronic and Systems,1997

4. Further passivity results for the attitude control problem;Tsiotras;IEEE Transactions on Automatic Control,1998

5. Input-to-state stable attitude control;Hokayem;Journal of Guidance, Control, and Dynamics,2008

Cited by 58 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Adaptive position tracking control of the lower limb exoskeleton robot with an uncertain dynamic model;2023 IEEE 18th Conference on Industrial Electronics and Applications (ICIEA);2023-08-18

2. Applied Optimal Control of Spacecraft Simulator Subject to Failures of Reaction Wheels;Arabian Journal for Science and Engineering;2023-06-08

3. Introduction;Intelligent Control and Learning Systems;2023

4. Adaptive neural fault-tolerant control of a quadrotor UAV via fast terminal sliding mode;Aerospace Science and Technology;2022-10

5. Adaptive Barrier Fast Terminal Sliding Mode Actuator Fault Tolerant Control Approach for Quadrotor UAVs;Mathematics;2022-08-20

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3