Modelling of quad‐rotor dynamics and Hardware‐in‐the‐Loop simulation
Abstract The quadcopter as one of the UAV (Unmanned aerial vehicles) is inherently unstable, and has six degrees of freedom (6 DOF), while the number of control inputs is four. The present work presents a sequential methodology to analyze and explain the control mechanism of quadcopter‐UAV in academ...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2022-10-01
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| Series: | The Journal of Engineering |
| Online Access: | https://doi.org/10.1049/tje2.12152 |