doi.org/10.1016/j.ast.2022.107386

Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control

..., Yuanfei Gao
13
Aerospace Science and Technology5.80
Volume: 122, Pages: 107386 - 107386
Published: Feb 7, 2022
Paper Fields
Paper Details
Title
Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control
DOI
doi.org/10.1016/j.ast.2022.107386
Published Date
Feb 7, 2022
Journal
Aerospace Science and Technology
Volume
122
Pages
107386 - 107386
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