LPV controller design for the lateral-directional motion of re-entry vehicle

Fuyuto Terui; Taro Tsukamoto; Hiroyuki Kajiwara

doi:10.2514/6.1999-4138

LPV controller design for the lateral-directional motion of re-entry vehicle

Fuyuto Terui, Taro Tsukamoto, Hiroyuki Kajiwara

Ship and Marine Dynamics

Research output: Contribution to conference › Paper › peer-review

Abstract

The development of Japanese unmanned reentry vehicle which is a part of the reusable space transportation system using H-II A launch vehicle is in progress. Since its dynamical characteristics such as stability derivatives change during the flight, it’s not feasible to use a single attitude controller which covers all flight conditions. This paper considers the application of Linear parameter-varying (LPV) controller synthesis technique to the lateral-directional attitude control in the approach and landing phase. The robustness and the performance of the resulting LPV controller are investigated through linear analysis and nonlinear simulation.

Original language	English
Pages	988-994
Number of pages	7
DOIs	https://doi.org/10.2514/6.1999-4138
Publication status	Published - 1999
Event	Guidance, Navigation, and Control Conference and Exhibit, 1999 - Portland, United States Duration: Aug 9 1999 → Aug 11 1999

Other

Other	Guidance, Navigation, and Control Conference and Exhibit, 1999
Country/Territory	United States
City	Portland
Period	8/9/99 → 8/11/99

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Control and Systems Engineering
Electrical and Electronic Engineering

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10.2514/6.1999-4138

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title = "LPV controller design for the lateral-directional motion of re-entry vehicle",

abstract = "The development of Japanese unmanned reentry vehicle which is a part of the reusable space transportation system using H-II A launch vehicle is in progress. Since its dynamical characteristics such as stability derivatives change during the flight, it{\textquoteright}s not feasible to use a single attitude controller which covers all flight conditions. This paper considers the application of Linear parameter-varying (LPV) controller synthesis technique to the lateral-directional attitude control in the approach and landing phase. The robustness and the performance of the resulting LPV controller are investigated through linear analysis and nonlinear simulation.",

author = "Fuyuto Terui and Taro Tsukamoto and Hiroyuki Kajiwara",

note = "Publisher Copyright: {\textcopyright} 1999 The American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; Guidance, Navigation, and Control Conference and Exhibit, 1999 ; Conference date: 09-08-1999 Through 11-08-1999",

year = "1999",

doi = "10.2514/6.1999-4138",

language = "English",

pages = "988--994",

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AU - Terui, Fuyuto

AU - Tsukamoto, Taro

AU - Kajiwara, Hiroyuki

PY - 1999

Y1 - 1999

N2 - The development of Japanese unmanned reentry vehicle which is a part of the reusable space transportation system using H-II A launch vehicle is in progress. Since its dynamical characteristics such as stability derivatives change during the flight, it’s not feasible to use a single attitude controller which covers all flight conditions. This paper considers the application of Linear parameter-varying (LPV) controller synthesis technique to the lateral-directional attitude control in the approach and landing phase. The robustness and the performance of the resulting LPV controller are investigated through linear analysis and nonlinear simulation.

AB - The development of Japanese unmanned reentry vehicle which is a part of the reusable space transportation system using H-II A launch vehicle is in progress. Since its dynamical characteristics such as stability derivatives change during the flight, it’s not feasible to use a single attitude controller which covers all flight conditions. This paper considers the application of Linear parameter-varying (LPV) controller synthesis technique to the lateral-directional attitude control in the approach and landing phase. The robustness and the performance of the resulting LPV controller are investigated through linear analysis and nonlinear simulation.

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T2 - Guidance, Navigation, and Control Conference and Exhibit, 1999

Y2 - 9 August 1999 through 11 August 1999

ER -

LPV controller design for the lateral-directional motion of re-entry vehicle

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