Linear quadratic optimal guidance with obstacle avoidance

Martin Weiss, Tal Shima

Research output: Contribution to conferencePaperpeer-review

Abstract

The paper applies linear quadratic optimal control to the problem of intercepting a maneuvering target while avoiding a static obstacle by a specified avoidance distance. The guidance law is expressed as the classical (augmented) proportional navigation type guidance, with optimal effort performance, with an additional correction term that achieves obstacle avoidance. The minimum avoidance distance is a parameter of the guidance algorithm. The performance of the guidance algorithm is illustrated using simulation results, both on the ideal, linear intercept model, that is used for guidance algorithm derivation, as on the more realistic nonlinear kinematics intercept model.

Original languageEnglish
StatePublished - 2017
Event57th Israel Annual Conference on Aerospace Sciences, IACAS 2017 - Tel Aviv and Haifa, Israel
Duration: 15 Mar 201716 Mar 2017

Conference

Conference57th Israel Annual Conference on Aerospace Sciences, IACAS 2017
Country/TerritoryIsrael
CityTel Aviv and Haifa
Period15/03/1716/03/17

ASJC Scopus subject areas

  • Aerospace Engineering

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