L1 adaptive controller for a missile longitudinal autopilot design

Jiang Wang, Chengyu Cao, Naira Hovakimyan, Richard E. Hindman, D. Brett Ridgely

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

Abstract

This paper considers application of L\ adaptive output feedback controller to a missile longitudinal autopilot design. The proposed adaptive controller has satisfactory performance in the presence of parametric uncertainties and time-varying disturbances. Simulations demonstrate the benefits of the control method and compare the results to Linear Quadratic Regulator (LQR) and Linear Quadratic Gaussian (LQG) with Loop Transfer Recovery (LTR) design.

Original languageEnglish (US)
Title of host publicationAIAA Guidance, Navigation and Control Conference and Exhibit
StatePublished - 2008
EventAIAA Guidance, Navigation and Control Conference and Exhibit - Honolulu, HI, United States
Duration: Aug 18 2008Aug 21 2008

Publication series

NameAIAA Guidance, Navigation and Control Conference and Exhibit

Other

OtherAIAA Guidance, Navigation and Control Conference and Exhibit
Country/TerritoryUnited States
CityHonolulu, HI
Period8/18/088/21/08

ASJC Scopus subject areas

  • Aerospace Engineering
  • Control and Systems Engineering

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