Active Vibration Control of a Maneuvering Flexible Spacecraft Using Hybrid Actuators: A Lyapunov-Based Control Approach
This paper presents a study concerning active vibration control of a smart flexible spacecraft during attitude maneuver using thrusters and reaction wheels (RW) in combination and piezoelectric (PZT) sensor/actuator patches. The large-angle maneuver and residual vibration of the spacecraft are contr...
| Main Authors: | , |
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| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2022-06-01
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| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_122467_956d536ec3dac5abc6fa0d414ea77b4c.pdf |