Full-state autopilot-guidance design under a linear quadratic differential game formulation

Maital Levy, Tal Shima, Shaul Gutman

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

Abstract

Full-state single-loop and full-state two-loop autopilot-guidance designs are derived using a linear quadratic differential game formulation. To keep all the states at reasonable values throughout the end-game, a cost function that includes appropriate running cost terms on some of the states is proposed. It is proven that the two designs may be identical under a linear quadratic differential game formulation and the proposed cost function. The theorem and guidance laws are illustrated using an interceptor missile having forward and aft controls.

Original languageEnglish
Title of host publication19th IFAC World Congress IFAC 2014, Proceedings
EditorsEdward Boje, Xiaohua Xia
Pages3942-3947
Number of pages6
ISBN (Electronic)9783902823625
DOIs
StatePublished - 2014
Event19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014 - Cape Town, South Africa
Duration: 24 Aug 201429 Aug 2014

Publication series

NameIFAC Proceedings Volumes (IFAC-PapersOnline)
Volume19

Conference

Conference19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014
Country/TerritorySouth Africa
CityCape Town
Period24/08/1429/08/14

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering

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