Anti-windup active disturbance rejection control of tiltable-rotors fully-actuated hexarotor
Tiltable-rotors fully-actuated unmanned aerial vehicles achieve full control by dynamically adjusting thrust vector direction through tilting mechanisms. However, physical constraints on actuator amplitudes and rates lead to noticeable actuator saturation effects. Such saturation can cause the thrus...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2025-05-01
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| Series: | International Journal of Advanced Robotic Systems |
| Online Access: | https://doi.org/10.1177/17298806251331321 |
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