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Attitude Control System Design of 3U CubeSat with Electrodynamic Tether for Post Mission Disposal Demonstration.
Naoya Shiraishi
Yuji Sato
Yoshihiko Shibuya
Shinya Fujita
Toshinori Kuwahara
Daisuke Suzuki
Published in:
SII (2022)
Keyphrases
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control system
real time control
case study
engineering design
design process
neural network
intelligent control
design decisions
computer aided
artificial intelligence
mathematical model
design principles
building blocks
control scheme
vision system
controller design
real time
space shuttle