Composite Guidance Law Against Maneuvering Target Considering Impact Angle Constraints
Author:
Affiliation:
1. Beijing Institute of Technology,School of Aerospace Engineering,Beijing,China,100081
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10401265/10401324/10401356.pdf?arnumber=10401356
Reference13 articles.
1. Three-dimensional terminal angle constraint finite-time dual-layer guidance law with autopilot dynamics
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4. Finite‐time extended state observer‐based exact tracking control of an unmanned surface vehicle
5. Three-Dimensional Diving Guidance for Hypersonic Gliding Vehicle via Integrated Design of FTNDO and AMSTSMC
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