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Control System Design for the Powered Ascent of Winged Rocket Based on Dynamic Inversion Theory.
Yuto Kitazono
Kazuki Kishiwada
Koichi Yonemoto
Takahiro Fujikawa
Takahiro Matsukami
Published in:
SICE (2021)
Keyphrases
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control system
conceptual framework
dynamic environments
design decisions
real time control
fuzzy logic
image reconstruction
engineering design
optimal design
intelligent control
design theory
real time
human computer interaction
design process
computational model
control scheme