Output-Constrained Adaptive Composite Nonsingular Terminal Sliding Mode Attitude Control for a Class of Spacecraft Systems with Mismatched Disturbances and Input Uncertainties

IF 1.5 4区工程技术 Q2 ENGINEERING, AEROSPACE

Journal of Aerospace Engineering Pub Date : 2024-01-01 DOI:10.1061/jaeeez.aseng-5027

Xin Ning, Yuan Zhu, Zheng Wang, Li Liu, Zhiwei Hao

引用次数: 0

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具有不匹配干扰和输入不确定性的一类航天器系统的输出受限自适应复合非奇异终端滑模姿态控制

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

Journal of Aerospace Engineering 工程技术-工程：土木

CiteScore

2.90

自引率

4.20%

发文量

149

审稿时长

6.4 months

期刊介绍： The Journal of Aerospace Engineering promotes the implementation and development of space and aerospace technologies and their transfer to other civil engineering applications. Topics of interest include aerodynamics, computational fluid dynamics, wind tunnel testing of buildings and structures, aerospace structures and materials, advanced composite materials, dynamics and control, real-time data acquisition, space engineering and construction, lunar base construction, field and remote sensing, and robotics.