Adaptive Fault-Tolerant Attitude Tracking Control of Spacecraft With Prescribed Performance

The science objectives of a spacecraft mission place stringent performance requirements on the spacecraft attitude control system. However, it remains an open problem how to guarantee consistent control performance necessary to meet these requirements, especially in the event of actuator faults and...

Full description

Saved in:
Bibliographic Details
Published inIEEE/ASME transactions on mechatronics Vol. 23; no. 1; pp. 331 - 341
Main Authors Hu, Qinglei, Shao, Xiaodong, Guo, Lei
Format Journal Article
LanguageEnglish
Published IEEE 01.02.2018
Subjects
Online AccessGet full text

Cover

Loading…