Martin T. Ozimek, Ph.D.

Affiliations: 
2010 Aeronautics and Astronautics Purdue University, West Lafayette, IN, United States 
Area:
Aerospace Engineering
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"Martin Ozimek"

Parents

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Kathleen Howell grad student 2010 Purdue
 (Low-thrust trajectory design and optimization of lunar south pole coverage missions.)
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Publications

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Sarli BV, Atchison JA, Ozimek MT, et al. (2019) Double Asteroid Redirection Test Mission: Heliocentric Phase Trajectory Analysis Journal of Spacecraft and Rockets. 56: 546-558
Ellison DH, Conway BA, Englander JA, et al. (2018) Analytic Gradient Computation for Bounded-Impulse Trajectory Models Using Two-Sided Shooting. Journal of Guidance, Control, and Dynamics : a Publication of the American Institute of Aeronautics and Astronautics Devoted to the Technology of Dynamics and Control. 41: 1449-1462
Atchison JA, Ozimek MT, Kantsiper BL, et al. (2016) Trajectory options for the DART mission Acta Astronautica. 123: 330-339
Scott CJ, Ozimek MT. (2013) Ongoing mission analysis for the solar TErrestrial RElations Observatory (stereo) Advances in the Astronautical Sciences. 148: 4013-4032
Ozimek MT, Scott CJ, Adams EY, et al. (2012) Mission design and systems architectures for a Venus orbiter and entry probe Aiaa Space Conference and Exposition 2012
Scott CJ, Ozimek MT. (2012) Optimal transfer and science orbit design in the proximity of small bodies Advances in the Astronautical Sciences. 142: 3391-3410
Grebow DJ, Ozimek MT, Howell KC. (2011) Design of optimal low-thrust lunar pole-sitter missions Journal of the Astronautical Sciences. 58: 55-79
Grebow DJ, Ozimek MT, Howell KC. (2011) Design of optimal low-thrust lunar pole-sitter missions Journal of the Astronautical Sciences. 58: 55-79
Stuart JR, Ozimek MT, Howellz KC. (2010) Optimal, low-thrust, path-constrained transfers between libration point orbits using invariant manifolds Aiaa/Aas Astrodynamics Specialist Conference 2010
Ozimek MT, Howell KC. (2010) Low-thrust transfers in the earth-moon system, including applications to libration point orbits Journal of Guidance, Control, and Dynamics. 33: 533-549
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