XÂY DỰNG THUẬT TOÁN XÁC ĐỊNH LUẬT ĐIỀU KHIỂN CHO UAV TRI-ROTORS TRÊN CƠ SỞ ỨNG DỤNG LÝ THUYẾT ĐIỀU KHIỂN TRƯỢT

Thành

BUILDING THE OPERATION OF DETERMINING THE CONTROL LAW FOR TRI-ROTORS UAV ON THE BASIS OF THE APPLICATION OF SLIDING CONTROL THEORY

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Authors

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

Keywords:

Tri-rotors UAV; Sliding control.

Abstract

The paper presents a sliding mode control solution for tri-rotors UAV to follow the reguired trajectory and posture. The sliding mode control laws are resistant to interference and ensure the required tracking accuracy even if there are parameter errors in the model describing tri-rotors UAV.

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Published

12-06-2020

How to Cite

Thành. “BUILDING THE OPERATION OF DETERMINING THE CONTROL LAW FOR TRI-ROTORS UAV ON THE BASIS OF THE APPLICATION OF SLIDING CONTROL THEORY”. Journal of Military Science and Technology, no. 67, June 2020, pp. 3-12, https://online.jmst.info/index.php/jmst/article/view/206.