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

Fuyuto Terui, Taro Tsukamoto, Hiroyuki Kajiwara

Research output: Contribution to conferencePaperpeer-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 languageEnglish
Pages988-994
Number of pages7
Publication statusPublished - 1999
EventGuidance, Navigation, and Control Conference and Exhibit, 1999 - Portland, United States
Duration: Aug 9 1999Aug 11 1999

Other

OtherGuidance, Navigation, and Control Conference and Exhibit, 1999
CountryUnited States
CityPortland
Period8/9/998/11/99

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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