Design of linear quadratic regulator (LQR) control system for flight stability of LSU-05

Heri Purnawan; Eko Budi Purwanto

doi:10.1088/1742-6596/890/1/012056

Design of linear quadratic regulator (LQR) control system for flight stability of LSU-05

Heri Purnawan, Mardlijah, Eko Budi Purwanto

Laboratory of Mathematical Modeling and System Simulation

Research output: Contribution to journal › Conference article › peer-review

25 Citations (Scopus)

Abstract

Lapan Surveillance UAV-05 (LSU-05) is an unmanned aerial vehicle designed to cruise time in 6 hours and cruise velocity about 30 m/s. Mission of LSU-05 is surveillance for researchs and observations such as traffics and disaster investigations. This paper aims to design a control system on the LSU-05 to fly steadily. The methods used to stabilize LSU-05 is Linear Quadratic Regulator (LQR). Based on LQR controller, there is obtained transient response for longitudinal motion, t_d = 0.221s, t_r = 0.419s, t_s = 0.719s, t_p = 1.359s, and M_p = 0%. In other hand, transient response for lateral-directional motion showed that t_d = 0.186s, t_r = 0.515s, t_s = 0.87s, t_p = 2.02s, and M_p = 0%. The result of simulation showed a good performance for this method.

Original language	English
Article number	012056
Journal	Journal of Physics: Conference Series
Volume	890
Issue number	1
DOIs	https://doi.org/10.1088/1742-6596/890/1/012056
Publication status	Published - 21 Sept 2017
Event	1st International Conference on Applied and Industrial Mathematics and Statistics 2017, ICoAIMS 2017 - Kuantan, Pahang, Malaysia Duration: 8 Aug 2017 → 10 Aug 2017

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title = "Design of linear quadratic regulator (LQR) control system for flight stability of LSU-05",

abstract = "Lapan Surveillance UAV-05 (LSU-05) is an unmanned aerial vehicle designed to cruise time in 6 hours and cruise velocity about 30 m/s. Mission of LSU-05 is surveillance for researchs and observations such as traffics and disaster investigations. This paper aims to design a control system on the LSU-05 to fly steadily. The methods used to stabilize LSU-05 is Linear Quadratic Regulator (LQR). Based on LQR controller, there is obtained transient response for longitudinal motion, td = 0.221s, tr = 0.419s, ts = 0.719s, tp = 1.359s, and Mp = 0%. In other hand, transient response for lateral-directional motion showed that td = 0.186s, tr = 0.515s, ts = 0.87s, tp = 2.02s, and Mp = 0%. The result of simulation showed a good performance for this method.",

author = "Heri Purnawan and Mardlijah and Purwanto, {Eko Budi}",

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AU - Purnawan, Heri

AU - Mardlijah,

AU - Purwanto, Eko Budi

N1 - Publisher Copyright: © Published under licence by IOP Publishing Ltd.

PY - 2017/9/21

Y1 - 2017/9/21

N2 - Lapan Surveillance UAV-05 (LSU-05) is an unmanned aerial vehicle designed to cruise time in 6 hours and cruise velocity about 30 m/s. Mission of LSU-05 is surveillance for researchs and observations such as traffics and disaster investigations. This paper aims to design a control system on the LSU-05 to fly steadily. The methods used to stabilize LSU-05 is Linear Quadratic Regulator (LQR). Based on LQR controller, there is obtained transient response for longitudinal motion, td = 0.221s, tr = 0.419s, ts = 0.719s, tp = 1.359s, and Mp = 0%. In other hand, transient response for lateral-directional motion showed that td = 0.186s, tr = 0.515s, ts = 0.87s, tp = 2.02s, and Mp = 0%. The result of simulation showed a good performance for this method.

AB - Lapan Surveillance UAV-05 (LSU-05) is an unmanned aerial vehicle designed to cruise time in 6 hours and cruise velocity about 30 m/s. Mission of LSU-05 is surveillance for researchs and observations such as traffics and disaster investigations. This paper aims to design a control system on the LSU-05 to fly steadily. The methods used to stabilize LSU-05 is Linear Quadratic Regulator (LQR). Based on LQR controller, there is obtained transient response for longitudinal motion, td = 0.221s, tr = 0.419s, ts = 0.719s, tp = 1.359s, and Mp = 0%. In other hand, transient response for lateral-directional motion showed that td = 0.186s, tr = 0.515s, ts = 0.87s, tp = 2.02s, and Mp = 0%. The result of simulation showed a good performance for this method.

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T2 - 1st International Conference on Applied and Industrial Mathematics and Statistics 2017, ICoAIMS 2017

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ER -

Design of linear quadratic regulator (LQR) control system for flight stability of LSU-05

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