Sliding mode control with tanh function for quadrotor UAV altitude and attitude stabilization
This paper addresses the problem of robust altitude (z), and attitude (?, ?, ?) control of ‘ ×’ mode configuration quadrotor UAV using a sliding mode control (SMC) with tanh function. The dynamic quadrotor model is derived by considering the nonlinearity factor. The dynamic model is simulated in MAT...
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| Main Authors: | , , |
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| Format: | Conference or Workshop Item |
| Published: |
2021
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| Subjects: | |
| Online Access: | http://eprints.utm.my/id/eprint/96893/ http://dx.doi.org/10.1007/978-981-16-0866-7_41 |
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