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Optimal proportional navigation guidance based on generalized predictive control

  • Beihang University

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

Abstract

A new form of Proportional Navigation Guidance (PNG) law for tactical missiles based on generalized nonlinear predictive control approach is proposed. A cost function with built-in integral action as well as optional control order has been introduced to improve the prediction performance. The flight-control system dynamics is also involved in formulation derivation. The performance of the new guidance law is demonstrated by simulation. The results show that the proposed guidance law is very effective against a highly maneuvering target.

Original languageEnglish
Title of host publication2012 16th International Conference on System Theory, Control and Computing, ICSTCC 2012 - Joint Conference Proceedings
StatePublished - 2012
Event2012 16th International Conference on System Theory, Control and Computing, ICSTCC 2012 - Sinaia, Romania
Duration: 12 Oct 201214 Oct 2012

Publication series

Name2012 16th International Conference on System Theory, Control and Computing, ICSTCC 2012 - Joint Conference Proceedings

Conference

Conference2012 16th International Conference on System Theory, Control and Computing, ICSTCC 2012
Country/TerritoryRomania
CitySinaia
Period12/10/1214/10/12

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