Approximate Analytical Solution of the Multiple Revolution Lambert’s Targeting ProblemClaudio Bombardelli, Javier Roa, Juan Luis Gonzalo|Journal of Guidance Control and Dynamics|2018Cited by 24
Mission analysis for the ion beam deflection of fictitious asteroid 2015 PDCClaudio Bombardelli, Juan Luis Cano, Davide Amato|Acta Astronautica|2015Cited by 17
Approximate solutions of non-linear circular orbit relative motion in curvilinear coordinatesClaudio Bombardelli, Javier Roa, Juan Luis Gonzalo|Celestial Mechanics and Dynamical Astronomy|2016Cited by 11
GNC Design for Asteroid Orbit Modification MissionsMiguel Hagenfeldt, Andrés Gálvez, Eleonora Luraschi et al.|AIAA Guidance, Navigation, and Control (GNC) Conference|2013Cited by 1
Quantification of the performance of numerical orbit propagatorsHodei Urrutxua, Claudio Bombardelli, Javier Roa et al.|LA Referencia (Red Federada de Repositorios Institucionales de Publicaciones Científicas)|2016Cited by 0