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Near Optimal Explicit Guidance Law with Impact Angle Constraints for a Hypersonic Re-entry Vehicle
Author(s) -
Karthikeyan Kalirajan,
Ashok Joshi
Publication year - 2018
Publication title -
incas buletin
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.282
H-Index - 10
eISSN - 2247-4528
pISSN - 2066-8201
DOI - 10.13111/2066-8201.2018.10.2.5
Subject(s) - hypersonic speed , atmospheric entry , aerospace engineering , angle of attack , computer science , engineering , aerodynamics

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