Balanced prescribed-distance guidance with impact angle constraint and input saturation-Reference-Cited by-同舟云学术

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Balanced prescribed-distance guidance with impact angle constraint and input saturation

Published:2024-03 Issue:4 Volume:361 Page:106640
ISSN:0016-0032
Container-title:Journal of the Franklin Institute
language:en
Short-container-title:Journal of the Franklin Institute

Author:

Wang Haibin^ORCID,You Bo,Wang Peng^ORCID,Xie Wenbo

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Postdoctoral Research Foundation of China

Publisher

Elsevier BV

Reference24 articles.

1. Tactical and Strategic Missile Guidance;Zarchan,2012

2. Applied Optimal Control;Bryson,1969

3. Optimal guidance laws with terminal impact angle constraint;Ryoo;J. Guid. Control Dyn.,2005

4. Time-to-go weighted optimal guidance with impact angle constraints;Ryoo;IEEE Trans. Control Syst. Technol.,2006

5. Generalized formulation of weighted optimal guidance laws with impact angle constraint;Lee;IEEE Trans. Aerosp. Electron. Syst.,2013

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