Actuator fault detection and isolation on a quadrotor unmanned aerial vehicle modeled as a linear parameter-varying system
This paper presents the design of a fault detection and diagnosis system for a quadrotor unmanned aerial vehicle under partial or total actuator fault. In order to control the quadrotor, the dynamic system is divided in two subsystems driven by the translational and the rotational dynamics, where th...
| Main Authors: | , , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2019-11-01
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| Series: | Measurement + Control |
| Online Access: | https://doi.org/10.1177/0020294018824764 |