Optimal Impulsive Collision Avoidance in Low Earth Orbit-Reference-Cited by-同舟云学术

Optimal Impulsive Collision Avoidance in Low Earth Orbit

Published:2015-02 Issue:2 Volume:38 Page:217-225
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Bombardelli Claudio¹,Hernando-Ayuso Javier¹

Affiliation:

1. Department of Aeronautical Engineering, Universidad Politécnica de Madrid, E-28040 Madrid, Spain

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G000742

Reference12 articles.

1. KlinkradH., Space Debris: Models and Risk Analysis, Springer–Verlag, New York, 2006, pp. 213–240.

2. AlfanoS. “Collision Avoidance Maneuver Planning Tool,” 15th AAS/AIAA Astrodynamics Specialist Conference, American Astronautical Soc. Paper 2005-308, 2005.

3. Analytical formulation of impulsive collision avoidance dynamics

4. Near-Optimal Deflection of Earth-Approaching Asteroids

5. ChanF. K., Spacecraft Collision Probability, Aerospace Press, El Segundo, CA, 2008, pp. 13–97, 47–61.

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