Optimal attitude planning along torque equilibrium points using aerodynamic database for deorbiting large space debris

Author:

Sasaki TakahiroORCID,Nakamura RyoORCID,Okamoto Hiroyuki

Funder

Japan Society for the Promotion of Science

Publisher

Elsevier BV

Reference22 articles.

1. J.-C. Liou, The Near-Earth Orbital Debris Problem and the Challenges for Environment Remediation, in: The 3rd International Space World Conference, Frankfurt, Germany, 2012.

2. Identifying the 50 statistically-most-concerning derelict objects in LEO;McKnight;Acta Astronaut.,2021

3. H. Okamoto, T. Yamamoto, A Novel Concept of Cost-Effective Active Debris Removal Spacecraft System, in: 1st International Orbital Debris Conference, Sugar Land, Texas, USA, 2019.

4. Thrust vector control of upper stage with a gimbaled thruster during orbit transfer;Wang;Acta Astronaut.,2016

5. Adaptive control/steering design for deorbiting space debris with hybrid actuators configuration;Sasaki,2023

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