Nonlinear three dimensional all-aspect guidance with terminal impact angle constraints
Author:
Funder
Basic and Applied Basic Research Foundation of Guangdong Province
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference31 articles.
1. Optimal control based guidance law to control both impact time and impact angle;Chen;Aerosp. Sci. Technol.,2019
2. Nonlinear optimal impact-angle-constrained guidance with large initial heading error;Li;J. Guid. Control Dyn.,2021
3. Impact time and angle control optimal guidance with field-of-view constraint;Chen;J. Guid. Control Dyn.,2022
4. Impact angle guidance using state-dependent (differential) Riccati equation: unified applicability analysis;Lin;J. Guid. Control Dyn.,2020
5. Nonlinear suboptimal guidance law with impact angle constraint: an sdre-based approach;Wang;IEEE Trans. Aerosp. Electron. Syst.,2020
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