Spacecraft robust attitude control attitude control with saturation nonlinearity

Long Life Show, Jyh Ching Juang, Ying Wen Jan, Chen Tsung Lin

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Citations (Scopus)

Abstract

The paper presents a robust nonlinear H control design method for rigid spacecraft asymptotic attitude control with input saturation nonlinearity. The solution of the nonlinear H control problem is known to related to the existence of solution to a Hamilton-Jacobi partially differential inequality (HJPDI). The papers proposes a candidate solution to the HJPDI for spacecraft attitude control that is subject to nonlinear dynamics and input saturation. The method is applied to the ROCSAT-3 attitude control problem to verify its effectiveness.

Original languageEnglish
Title of host publicationAIAA Guidance, Navigation, and Control Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624101083
Publication statusPublished - 2002 Jan 1
EventAIAA Guidance, Navigation, and Control Conference and Exhibit 2002 - Monterey, CA, United States
Duration: 2002 Aug 52002 Aug 8

Publication series

NameAIAA Guidance, Navigation, and Control Conference and Exhibit

Other

OtherAIAA Guidance, Navigation, and Control Conference and Exhibit 2002
CountryUnited States
CityMonterey, CA
Period02-08-0502-08-08

All Science Journal Classification (ASJC) codes

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

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