Eigenvalue assignment based on standard characteristic polynominal in design of aircraft control systems

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

Abstract

Design method of eigenvalue assignment based on standard characteristic polynomial, as well as mathematical solving process of the method, is proposed in this paper so as to resolve the uncertainty of ideal eigenvalue choice in modern control theory and the difficultly in engineering implementation of modern control system design methods. Longitudinal stability holding control system of an aircraft was designed and simulated by employing proposed method. Dynamic character and robust performance simulation of the system are given. Simulation results show that the method achieves the control quality and has better robustness than another method. There is only one design parameter which is easy to calculate. So, the method is characterized as simple design, logical structure, easy programming and convenient for engineering implementation.

Original languageEnglish
Title of host publicationSeventh International Symposium on Instrumentation and Control Technology
Subtitle of host publicationMeasurement Theory and Systems and Aeronautical Equipment
DOIs
StatePublished - 2008
Event7th International Symposium on Instrumentation and Control Technology: Measurement Theory and Systems and Aeronautical Equipment - Beijing, China
Duration: 10 Oct 200813 Oct 2008

Publication series

NameProceedings of SPIE - The International Society for Optical Engineering
Volume7128
ISSN (Print)0277-786X

Conference

Conference7th International Symposium on Instrumentation and Control Technology: Measurement Theory and Systems and Aeronautical Equipment
Country/TerritoryChina
CityBeijing
Period10/10/0813/10/08

Keywords

  • Aircraft control
  • Eigenvalue assignment
  • Standard characteristic polynomial

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