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Vladimir Martinusi
Vladimir Martinusi
Faculty of Aerospace Engineering – Technion, Israel Intitute of Technology
Verified email at technion.ac.il - Homepage
Title
Cited by
Cited by
Year
Solutions and periodicity of satellite relative motion under even zonal harmonics perturbations
V Martinuşi, P Gurfil
Celestial Mechanics and Dynamical Astronomy 111, 387-414, 2011
592011
Relative spacecraft motion in a central force field
D Condurache, V Martinuşi
Journal of Guidance, Control, and Dynamics 30 (3), 873-876, 2007
462007
Foucault Pendulum-like problems: A tensorial approach
D Condurache, V Martinusi
International Journal of Non-Linear Mechanics 43 (8), 743-760, 2008
442008
Quaternionic exact solution to the relative orbital motion problem
D Condurache, V Martinusi
Journal of guidance, control, and dynamics 33 (4), 1035-1047, 2010
352010
Kepler's problem in rotating reference frames Part II: relative orbital motion
D Condurache, V Martinusi
Journal of Guidance, Control, and Dynamics 30 (1), 201-213, 2007
342007
Kepler's problem in rotating reference frames part i: Prime integrals, vectorial regularization
D Condurache, V Martinusi
Journal of Guidance, Control, and Dynamics 30 (1), 192-200, 2007
312007
Exact solution to the relative orbital motion in eccentric orbits
D Condurache, V Martinuşi
Solar System Research 43 (1), 41-52, 2009
252009
A complete closed form vectorial solution to the Kepler problem
D Condurache, V Martinuşi
Meccanica 42 (5), 465-476, 2007
242007
Analytic propagation of near-circular satellite orbits in the atmosphere of an oblate planet
V Martinusi, L Dell’Elce, G Kerschen
Celestial Mechanics and Dynamical Astronomy 123, 85-103, 2015
202015
Exact solution to the relative orbital motion in a central force field
D Condurache, V Martinusi
2008 2nd International Symposium on Systems and Control in Aerospace and …, 2008
182008
A novel hypercomplex solution to Kepler’s problem
D Condurache, V Martinusi
Publications of the Astronomy Department of the Eötvös University (PADEU) 19 …, 2007
142007
Hypercomplex eccentric anomaly in the unified solution to the relative orbital motion
D Condurache, V Martinusi
Advances in the Astronautical Sciences 135 (1), 281-300, 2009
122009
First-order analytic propagation of satellites in the exponential atmosphere of an oblate planet
V Martinusi, L Dell’Elce, G Kerschen
Celestial Mechanics and Dynamical Astronomy 127, 451-476, 2017
102017
Robust optimal rendezvous using differential drag
L Dell'Elce, V Martinusi, G Kerschen
AIAA/AAS astrodynamics specialist conference, 4161, 2014
92014
Analytical solutions for J 2-perturbed unbounded equatorial orbits
V Martinusi, P Gurfil
Celestial Mechanics and Dynamical Astronomy 115, 35-57, 2013
72013
Analytical Derivation of Single-Impulse Maneuvers Guaranteeing Bounded Relative Motion Under
V Martinusi, P Gurfil
Journal of Guidance, Control, and Dynamics 37 (1), 233-242, 2014
62014
Analytical Orbit Propagator Based on Vectorial Orbital Elements
D Condurache, V Martinusi
42012
A Quaternionic Exact Solution to the Relative Orbital Motion
D Condurache, V Martinusi
AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 6764, 2008
42008
A Tensorial Explicit Solution to Darboux Equation
D Condurache, V Martinusi
The 2nd International Conference” Advanced Concepts in Mechanical Engineering, 2006
42006
Universal functions in the study of the relative orbital dynamics
D Condurache, V Martinusi
Advances in the Astronautical Sciences 145, 881-892, 2012
32012
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