Suboptimal guidance law against maneuvering target with time and angle constraints-Reference-Cited by-同舟云学术

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Suboptimal guidance law against maneuvering target with time and angle constraints

Published:2024-05 Issue: Volume:148 Page:109111
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Xie Jiliang,Ma Kemao^ORCID

Publisher

Elsevier BV

Reference39 articles.

1. Tactical and strategic missile guidance;Zarchan,2006

2. Distributed cooperative guidance for multivehicle simultaneous arrival without numerical singularities;Li;J. Guidance Control Dyn.,2020

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

4. Optimality of linear time-varying guidance for impact angle control;Lee;IEEE Trans. Aerosp. Electron. Syst.,2012

5. Optimal guidance around circular trajectories for impact-angle interception;Tsalik;J. Guidance Control Dyn.,2016

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