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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Bibliographic Details
Main Authors: Noordin, Aminurrashid, Mohd. Basri, Mohd. Ariffanan, Mohamed, Zaharuddin
Format: Conference or Workshop Item
Published: 2021
Subjects: