Surface-to-air missile autopilot design using LQG/LTR gain scheduling method

Jianqiao Yu*, Guanchen Luo, Yuesong Mei

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

14 Citations (Scopus)

Abstract

Linear quadratic Gaussian with loop transfer recovery (LQG/LTR) gain scheduling technique is utilized to design gain scheduling autopilot for surface-to-air missile. In order to eliminate the artificial uncertainties that the traditional "trial and error" design process introduces into system, a method to design target loop based on pole assignment is proposed, which provides an explicit algorithm to construct the matrix differential Riccati equation (MDRE) based on the expected poles determined by the performance specifications. Meanwhile, it is proved that by introducing integrators to augment plant dynamics the fast modes of LQG/LTR gain scheduling controller can be restrained effectively, which alleviates an obstacle for the engineering application of LQG/LTR gain scheduling technique. The proposed method is applied in the design of LQG/LTR gain scheduling autopilot for a surface-to-air missile. The design and simulation results indicate that the fast modes of controller are eliminated obviously, and that the dynamic characteristics of autopilot are stable when flight Mach number and altitude vary.

Original languageEnglish
Pages (from-to)279-286
Number of pages8
JournalChinese Journal of Aeronautics
Volume24
Issue number3
DOIs
Publication statusPublished - Jun 2011

Keywords

  • autopilot design
  • flight control
  • gain scheduling
  • loop transfer recovery
  • pole assignment

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