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...
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Published in | IEEE/ASME transactions on mechatronics Vol. 23; no. 1; pp. 331 - 341 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
IEEE
01.02.2018
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Subjects | |
Online Access | Get full text |
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