Impact time control with generalized look angle formulation under constraint

Raziye Tekin, Koray S. Erer, Florian Holzapfel

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

2 Scopus citations

Abstract

The nonlinear impact time control problem against stationary targets is investigated. The guidance law utilized in this paper is derived via shaping one of the fundamental states of the engagement. For that purpose, polynomial shaping of the look angle is considered. First, the boundary conditions of the engagement are introduced and the general form of the guidance law is presented. Afterwards, guidance gain determination for any order and the time domain solutions of the engagement are presented for the linearized kinematics. Later, the guidance law is modified for look angle constraint in an adaptive application scheme, which facilities closed loop application. The performance of the proposed guidance algorithm is demonstrated through simulations. In addition, a comparison study is held, whose results imply that the cubic polynomial is energy efficient for the look angle shaping.

Original languageEnglish
Title of host publicationAIAA Scitech 2019 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105784
DOIs
StatePublished - 2019
EventAIAA Scitech Forum, 2019 - San Diego, United States
Duration: 7 Jan 201911 Jan 2019

Publication series

NameAIAA Scitech 2019 Forum

Conference

ConferenceAIAA Scitech Forum, 2019
Country/TerritoryUnited States
CitySan Diego
Period7/01/1911/01/19

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