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The dynamics of asteroid deflection and manipulation using mass ejection are examined. First, a linearized small angular velocity and inertia tensor deviation model for close-to-principal-axis rota... Click to show full abstract
The dynamics of asteroid deflection and manipulation using mass ejection are examined. First, a linearized small angular velocity and inertia tensor deviation model for close-to-principal-axis rota...
Keywords:
manipulation;
mass ejection;
active mass;
deflection
Journal Title: Journal of Spacecraft and Rockets
Year Published: 2020
Link to full text (if available)
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Journal Title: Journal of Spacecraft and Rockets
Year Published: 2020
Link to full text (if available)
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recommendations!