Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint

An improved tentacle-based bank-angle transient method that requires less computation and provides effective feedback is proposed to offer a new choice for reentry gliding hypersonic vehicle maneuvering guidance. The longitudinal guidance strategy of hypersonic vehicles is applied to track standard...

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Bibliographic Details
Main Authors: Yang Gao, Guangbin Cai, Xiaogang Yang, Mingzhe Hou
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/8809704/