Control surface inverse algorithm and application to nonlinear H missile control

Chien Chung Kung, Ciann Dong Yang, Keng Lon Lei

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

1 Citation (Scopus)

Abstract

The proposed nonlinear H_inf missile autopilot in this paper is to resist maximal possible disturbances and counterbalance vortex-induced yawing moments during high AOA flight. The implementation of the nonlinear H_inf missile autopilot is solved by the control surface inverse algorithm (CSIA). The CSIA is an algorithm to compute the associated control surface deflections based on minimizing the global errors between the commands and actual control forces and moments. The derivations of the control law, the control surface inverse algorithm of the autopilot and the satisfying results of the heading reversal maneuver are demonstrated in this paper.

Original languageEnglish
Title of host publicationProceedings of the IEEE Conference on Decision and Control
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages5456-5461
Number of pages6
ISBN (Print)0780379241
DOIs
Publication statusPublished - 2003
Event42nd IEEE Conference on Decision and Control - Maui, HI, United States
Duration: 2003 Dec 92003 Dec 12

Publication series

NameProceedings of the IEEE Conference on Decision and Control
Volume5
ISSN (Print)0743-1546
ISSN (Electronic)2576-2370

Other

Other42nd IEEE Conference on Decision and Control
Country/TerritoryUnited States
CityMaui, HI
Period03-12-0903-12-12

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering
  • Modelling and Simulation
  • Control and Optimization

Fingerprint

Dive into the research topics of 'Control surface inverse algorithm and application to nonlinear H missile control'. Together they form a unique fingerprint.

Cite this