Zhao et al., 2022 - Google Patents
Rotation matrix-based finite-time attitude synchronization control for flexible spacecrafts with unknown inertial parameters and actuator faultsZhao et al., 2022
- Document ID
- 9375318629227459875
- Author
- Zhao H
- Wu X
- Xie Y
- Du Y
- Zhang Z
- Li Y
- Publication year
- Publication venue
- ISA transactions
External Links
Snippet
This paper studies the distributed attitude synchronization control for flexible spacecrafts with the consideration of unmeasurable modal variable and partial loss of actuator effectiveness faults. The designed rotation matrix-based controller consisted of the basic …
- 239000011159 matrix material 0 title abstract description 33
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