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...

全面介紹

Saved in:
書目詳細資料
Main Authors: Noordin, Aminurrashid, Mohd. Basri, Mohd. Ariffanan, Mohamed, Zaharuddin
格式: Conference or Workshop Item
出版: 2021
主題:
在線閱讀:http://eprints.utm.my/id/eprint/96893/
http://dx.doi.org/10.1007/978-981-16-0866-7_41
標簽: 添加標簽
沒有標簽, 成為第一個標記此記錄!