Design of UAV Attitude Control Law Based on the OGPC

ZHANG Li-zhen; WANG Qing-yu; WANG Mi-mi; HUANG Li-wei; ZHENG Ying

doi:10.3969/j.issn.1671-637x.2017.04.006

Journals >Electronics Optics & Control >Volume 24 >Issue 4 >Page 19 > Article

Electronics Optics & Control
Vol. 24, Issue 4, 19 (2017)

Design of UAV Attitude Control Law Based on the OGPC

ZHANG Li-zhen, WANG Qing-yu, WANG Mi-mi, HUANG Li-wei, and ZHENG Ying

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[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2017.04.006 Cite this Article

ZHANG Li-zhen, WANG Qing-yu, WANG Mi-mi, HUANG Li-wei, ZHENG Ying. Design of UAV Attitude Control Law Based on the OGPC[J]. Electronics Optics & Control, 2017, 24(4): 19 Copy Citation Text

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Abstract

The Optimal Generalized Predictive Control (OGPC) algorithm is studied. The attitude of Unmanned Aerial Vehicle (UAV) is dived into two loops of fast and slow, OGPC is used respectively in the design of the two loops, and a simulation analysis is carried out. The results show that the UAV attitude control law based on OGPC has good control performance.

Keywords

attitude control Optimal Generalized Predictive Control (OGPC)Unmanned Aerial Vehicle (UAV)

ZHANG Li-zhen, WANG Qing-yu, WANG Mi-mi, HUANG Li-wei, ZHENG Ying. Design of UAV Attitude Control Law Based on the OGPC[J]. Electronics Optics & Control, 2017, 24(4): 19

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