XÂY DỰNG MÔ HÌNH ĐIỀU KHIỂN CHUYỂN ĐỘNG  DẠNG AFFINE CHO UAV TRI-ROTORS

Thành

AFFINE MOTION CONTROL MODEL FOR UAV TRI-ROTORS

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Authors

Dang Van Thanh (Corresponding Author) Academy of Military Science and Technology

Keywords:

Tri-rotor; UAV; Roll; Pitch; Yaw; Affine; Dynamics.

Abstract

In this paper, the Tri-rotor dynamical model to transform it to affine form control system model, which is easier to apply the modern control theories to synthesize the Tri-rotor UAV control law is analyzed. A specific Tri-rotor UAV’s model is selected, the Matlab-Simulink to simulate the steady-state motion in space to demonstrate the correctness of this model is used.

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Published

10-04-2020

How to Cite

Thành. “AFFINE MOTION CONTROL MODEL FOR UAV TRI-ROTORS”. Journal of Military Science and Technology, no. 66, Apr. 2020, pp. 16-24, https://en.jmst.info/index.php/jmst/article/view/221.