[HTML][HTML] Nonlinear model predictive control leveraging quantum-inspired optimization in the three body problem with uncertainty
F De Grossi, C Circi - Acta Astronautica, 2023 - Elsevier
The optimization and control of spacecraft trajectories in presence of uncertainties and
unmodeled disturbances represents a challenging problem. Future missions would benefit …
unmodeled disturbances represents a challenging problem. Future missions would benefit …
Trajectory optimization for the Horyu-VI international lunar mission
F De Grossi, P Marzioli, M Cho, F Santoni, C Circi - Astrodynamics, 2021 - Springer
The Horyu-VI nano-satellite is an international lunar mission with the purpose of studying the
lunar horizon glow (LHG)—a still unclear phenomenon caused by electrostatically charged …
lunar horizon glow (LHG)—a still unclear phenomenon caused by electrostatically charged …
Attitude Determination and Control System Design for a 3U CubeSat to Monitor Forward Light Scattering over Earth Horizon
M Esit, K Jeje, R Subsinchai, R Cordova, MA Pham… - kyutech.repo.nii.ac.jp
The design of the attitude determination and control system (ADCS) of CubeSats plays a
crucial role in the success of their missions. ADCS design is a challenging task for CubeSats …
crucial role in the success of their missions. ADCS design is a challenging task for CubeSats …