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Time Optimal State Feedback Control with Application to a Spacecraft with Cold Gas Propulsion * *This work was supported by NASA SBIR/STTR Phase II grant for the Free-Flying Unmanned Robotic Spacecraft for Asteroid Resource Prospecting and Characterization project under contract NNX15CK07C.
Kitchen-McKinley, Samuel J., Drakunov, Sergey V.Volume:
50
Language:
english
Journal:
IFAC-PapersOnLine
DOI:
10.1016/j.ifacol.2017.08.1366
Date:
July, 2017
File:
PDF, 1.13 MB
english, 2017