Aerodynamic surfaces control allocation for RLV reentry

Zhi Xu, Shuo Tang

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

3 Scopus citations

Abstract

In this paper, aerodynamic control surfaces of reusable launch vehicle (RLV) in reentry phase were converted into a constrained optimization problem, and using a mixed linear programming algorithm to solve them. For nonlinear between aerodynamic control surfaces and control torque, the piecewise linear programming algorithm was used to solve the control surfaces failure and on-line reconfigurable optimization problem. Finally, simulation verify three failure modes of aerodynamic surfaces by piecewise linear programming method and aerodynamic surfaces can be reconstructed with good performance and a smaller allocation error.

Original languageEnglish
Title of host publicationProceedings - 2010 2nd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2010
Pages73-76
Number of pages4
DOIs
StatePublished - 2010
Event2010 2nd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2010 - Nanjing, China
Duration: 26 Aug 201028 Aug 2010

Publication series

NameProceedings - 2010 2nd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2010
Volume1

Conference

Conference2010 2nd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2010
Country/TerritoryChina
CityNanjing
Period26/08/1028/08/10

Keywords

  • Aerodynamic control surfaces
  • Control allocation
  • Mixed integer linear programming
  • Reusable launch vehicle

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