Modeling and control of a stratospheric satellite

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Trajectory tracking control of a stratospheric satellite is investigated in this paper. A simplified dynamical model for the stratospheric satellite is established based on the Lagrange equation to design its longitudinal trajectory tracking controller. From the model it is proved that the tracking problem cannot be solved by direct input-output feedback linearization control strategy, so the stratospheric satellite model is decomposed into two subsystems and a controller composed by two serial feedback sub-controllers for these subsystems is presented. Simulation results illustrate the performance of the closed-loop system controlled by the proposed controller.

Original languageEnglish
Title of host publication2013 25th Chinese Control and Decision Conference, CCDC 2013
Pages811-815
Number of pages5
DOIs
StatePublished - 2013
Event2013 25th Chinese Control and Decision Conference, CCDC 2013 - Guiyang, China
Duration: 25 May 201327 May 2013

Publication series

Name2013 25th Chinese Control and Decision Conference, CCDC 2013

Conference

Conference2013 25th Chinese Control and Decision Conference, CCDC 2013
Country/TerritoryChina
CityGuiyang
Period25/05/1327/05/13

Keywords

  • Input-output feedback linearization
  • Modeling
  • Stratospheric satellite
  • Trajectory controllers

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