Event-triggered adaptive attitude tracking control for spacecraft with unknown actuator faults

• المؤلفون الرئيسيون: Wang, Chenliang, Guo, Lei, Wen, Changyun, Hu, Qinglei, Qiao, Jianzhong
• مؤلفون آخرون: School of Electrical and Electronic Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2022
• الموضوعات: Engineering::Electrical and electronic engineering; Adaptive Control; Uncertainties
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/155207

This paper is devoted to attitude tracking control of fractionated spacecraft with wireless communication. We consider the practical case that the spacecraft suffers from uncertain inertia parameters, external disturbances, and even unknown and time-varying actuator faults. Within the framework of t...