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
59 2011 Relative spacecraft motion in a central force field D Condurache, V Martinuşi
Journal of Guidance, Control, and Dynamics 30 (3), 873-876, 2007
46 2007 Foucault Pendulum-like problems: A tensorial approach D Condurache, V Martinusi
International Journal of Non-Linear Mechanics 43 (8), 743-760, 2008
44 2008 Quaternionic exact solution to the relative orbital motion problem D Condurache, V Martinusi
Journal of guidance, control, and dynamics 33 (4), 1035-1047, 2010
35 2010 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
34 2007 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
31 2007 Exact solution to the relative orbital motion in eccentric orbits D Condurache, V Martinuşi
Solar System Research 43 (1), 41-52, 2009
25 2009 A complete closed form vectorial solution to the Kepler problem D Condurache, V Martinuşi
Meccanica 42 (5), 465-476, 2007
24 2007 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
20 2015 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
18 2008 A novel hypercomplex solution to Kepler’s problem D Condurache, V Martinusi
Publications of the Astronomy Department of the Eötvös University (PADEU) 19 …, 2007
14 2007 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
12 2009 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
10 2017 Robust optimal rendezvous using differential drag L Dell'Elce, V Martinusi, G Kerschen
AIAA/AAS astrodynamics specialist conference, 4161, 2014
9 2014 Analytical solutions for J 2 -perturbed unbounded equatorial orbits V Martinusi, P Gurfil
Celestial Mechanics and Dynamical Astronomy 115, 35-57, 2013
7 2013 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
6 2014 Analytical Orbit Propagator Based on Vectorial Orbital Elements D Condurache, V Martinusi
4 2012 A Quaternionic Exact Solution to the Relative Orbital Motion D Condurache, V Martinusi
AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 6764, 2008
4 2008 A Tensorial Explicit Solution to Darboux Equation D Condurache, V Martinusi
The 2nd International Conference” Advanced Concepts in Mechanical Engineering, 2006
4 2006 Universal functions in the study of the relative orbital dynamics D Condurache, V Martinusi
Advances in the Astronautical Sciences 145, 881-892, 2012
3 2012