Stefano Campagnola
Stefano Campagnola
Europa Clipper Mission Design Manager, JPL
Verified email at
Cited by
Cited by
Endgame problem part 2: multibody technique and the Tisserand-Poincare graph
S Campagnola, RP Russell
Journal of Guidance, Control, and Dynamics 33 (2), 476-486, 2010
Small satellites for space science: A COSPAR scientific roadmap
RM Millan, R von Steiger, M Ariel, S Bartalev, M Borgeaud, ...
Advances in space research 64 (8), 1466-1517, 2019
Endgame problem part 1: V-infinity-leveraging technique and the leveraging graph
S Campagnola, RP Russell
Journal of Guidance, Control, and Dynamics 33 (2), 463-475, 2010
Lagrangian coherent structures in the planar elliptic restricted three-body problem
ES Gawlik, JE Marsden, PC Du Toit, S Campagnola
Celestial mechanics and dynamical astronomy 103, 227-249, 2009
Mission analysis for the Martian Moons Explorer (MMX) mission
S Campagnola, CH Yam, Y Tsuda, N Ogawa, Y Kawakatsu
Acta Astronautica 146, 409-417, 2018
Optimization of low-energy resonant hopping transfers between planetary moons
G Lantoine, RP Russell, S Campagnola
Acta Astronautica 68 (7-8), 1361-1378, 2011
Flybys in the planar, circular, restricted, three-body problem
S Campagnola, P Skerritt, RP Russell
Celestial Mechanics and Dynamical Astronomy 113, 343-368, 2012
Mission to earth–moon lagrange point by a 6u cubesat: Equuleus
R Funase, S Ikari, K Miyoshi, Y Kawabata, S Nakajima, S Nomura, ...
IEEE Aerospace and Electronic Systems Magazine 35 (3), 30-44, 2020
Stochastic differential dynamic programming with unscented transform for low-thrust trajectory design
N Ozaki, S Campagnola, R Funase, CH Yam
Journal of Guidance, Control, and Dynamics 41 (2), 377-387, 2018
EQUULEUS trajectory design
K Oguri, K Oshima, S Campagnola, K Kakihara, N Ozaki, N Baresi, ...
The Journal of the Astronautical Sciences 67 (3), 950-976, 2020
Low-thrust approach and gravitational capture at Mercury
R Jehn, S Campagnola, D Garcia, S Kemble
18th International Symposium on Space Flight Dynamics 548, 487, 2004
Subregions of motion and elliptic halo orbits in the elliptic restricted three-body problem
S Campagnola, M Lo, P Newton
Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space …, 2008
Science goals and mission architecture of the Europa lander mission concept
KP Hand, CB Phillips, A Murray, JB Garvin, EH Maize, RG Gibbs, ...
The Planetary Science Journal 3 (1), 22, 2022
Tisserand-leveraging transfers
S Campagnola, A Boutonnet, J Schoenmaekers, DJ Grebow, ...
Journal of Guidance, Control, and Dynamics 37 (4), 1202-1210, 2014
Tube stochastic optimal control for nonlinear constrained trajectory optimization problems
N Ozaki, S Campagnola, R Funase
Journal of Guidance, Control, and Dynamics 43 (4), 645-655, 2020
Generation of an optimum target trajectory for the TerraSAR-X repeat observation satellite
S D'Amico, C Arbinger, M Kirschner, S Campagnola
18th International Symposium on Space Flight Dynamics 548, 137, 2004
Neptune and Triton: Essential pieces of the Solar System puzzle
A Masters, N Achilleos, CB Agnor, S Campagnola, S Charnoz, ...
Planetary and Space Science 104, 108-121, 2014
Broad search for unstable resonant orbits in the planar circular restricted three-body problem
RL Anderson, S Campagnola, G Lantoine
Celestial Mechanics and Dynamical Astronomy 124, 177-199, 2016
Leveraging flybys of low mass moons to enable an enceladus orbiter
NJ Strange, S Campagnola, RP Russell
Advances in the Astronautical Sciences 135 (3), 2207-2225, 2009
Jovian tour design for orbiter and lander missions to Europa
S Campagnola, BB Buffington, AE Petropoulos
Acta Astronautica 100, 68-81, 2014
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