Nonlinear autopilot design based on inversion system and fuzzy logic

Haijun Li; Xianlin Huang; Xiaojun Ban

doi:10.1109/CHICC.2006.4347177

Nonlinear autopilot design based on inversion system and fuzzy logic

Haijun Li^*
, Xianlin Huang
, Xiaojun Ban

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Scopus citations

Abstract

The design specifications of the missile autopilot can be described by the expected behavior and in this paper one kind of nonlinear longitudinal controller is proposed based on dynamic inversion theory and multi-scales property of missile system. Further more, choosing Mach as a scheduling variable, the autopilot based on a Mamdani fuzzy controller is synthesized. Numerical simulations show the missile autopilot can achieve the performance goals and good robust performance over the whole flight envelope with uncertainty of aerodynamic parameters.

Original language	English
Title of host publication	Proceedings of the 26th Chinese Control Conference, CCC 2007
Pages	357-360
Number of pages	4
DOIs	https://doi.org/10.1109/CHICC.2006.4347177
State	Published - 2007
Event	26th Chinese Control Conference, CCC 2007 - Zhangjiajie, China Duration: 26 Jul 2007 → 31 Jul 2007

Publication series

Name	Proceedings of the 26th Chinese Control Conference, CCC 2007

Conference

Conference	26th Chinese Control Conference, CCC 2007
Country/Territory	China
City	Zhangjiajie
Period	26/07/07 → 31/07/07

Keywords

Autopilot
Dynamic inversion
Expected behavior
Fuzzy controller
Robust performance

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10.1109/CHICC.2006.4347177

Cite this

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title = "Nonlinear autopilot design based on inversion system and fuzzy logic",

abstract = "The design specifications of the missile autopilot can be described by the expected behavior and in this paper one kind of nonlinear longitudinal controller is proposed based on dynamic inversion theory and multi-scales property of missile system. Further more, choosing Mach as a scheduling variable, the autopilot based on a Mamdani fuzzy controller is synthesized. Numerical simulations show the missile autopilot can achieve the performance goals and good robust performance over the whole flight envelope with uncertainty of aerodynamic parameters.",

keywords = "Autopilot, Dynamic inversion, Expected behavior, Fuzzy controller, Robust performance",

author = "Haijun Li and Xianlin Huang and Xiaojun Ban",

year = "2007",

doi = "10.1109/CHICC.2006.4347177",

language = "英语",

isbn = "7900719229",

series = "Proceedings of the 26th Chinese Control Conference, CCC 2007",

pages = "357--360",

booktitle = "Proceedings of the 26th Chinese Control Conference, CCC 2007",

note = "26th Chinese Control Conference, CCC 2007 ; Conference date: 26-07-2007 Through 31-07-2007",

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AU - Li, Haijun

AU - Huang, Xianlin

AU - Ban, Xiaojun

PY - 2007

Y1 - 2007

N2 - The design specifications of the missile autopilot can be described by the expected behavior and in this paper one kind of nonlinear longitudinal controller is proposed based on dynamic inversion theory and multi-scales property of missile system. Further more, choosing Mach as a scheduling variable, the autopilot based on a Mamdani fuzzy controller is synthesized. Numerical simulations show the missile autopilot can achieve the performance goals and good robust performance over the whole flight envelope with uncertainty of aerodynamic parameters.

AB - The design specifications of the missile autopilot can be described by the expected behavior and in this paper one kind of nonlinear longitudinal controller is proposed based on dynamic inversion theory and multi-scales property of missile system. Further more, choosing Mach as a scheduling variable, the autopilot based on a Mamdani fuzzy controller is synthesized. Numerical simulations show the missile autopilot can achieve the performance goals and good robust performance over the whole flight envelope with uncertainty of aerodynamic parameters.

KW - Autopilot

KW - Dynamic inversion

KW - Expected behavior

KW - Fuzzy controller

KW - Robust performance

UR - https://www.scopus.com/pages/publications/37749053291

U2 - 10.1109/CHICC.2006.4347177

DO - 10.1109/CHICC.2006.4347177

M3 - 会议稿件

AN - SCOPUS:37749053291

SN - 7900719229

SN - 9787900719225

T3 - Proceedings of the 26th Chinese Control Conference, CCC 2007

SP - 357

EP - 360

BT - Proceedings of the 26th Chinese Control Conference, CCC 2007

T2 - 26th Chinese Control Conference, CCC 2007

Y2 - 26 July 2007 through 31 July 2007

ER -

Nonlinear autopilot design based on inversion system and fuzzy logic

Abstract

Publication series

Conference

Keywords

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