| 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 | 175 | 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 | 130 | 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 | 116 | 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 | 104 | 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 | 86 | 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 | 80 | 2011 |
| 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 | 79 | 2020 |
| 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 | 77 | 2022 |
| Flybys in the planar, circular, restricted, three-body problem S Campagnola, P Skerritt, RP Russell Celestial Mechanics and Dynamical Astronomy 113, 343-368, 2012 | 77 | 2012 |
| 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 | 75 | 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 | 71 | 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 | 65 | 2004 |
| 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 | 64 | 2020 |
| 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 | 62 | 2008 |
| Tisserand-leveraging transfers S Campagnola, A Boutonnet, J Schoenmaekers, DJ Grebow, ... Journal of Guidance, Control, and Dynamics 37 (4), 1202-1210, 2014 | 61 | 2014 |
| 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 | 52 | 2014 |
| Tour design techniques for the Europa Clipper mission S Campagnola, BB Buffington, T Lam, AE Petropoulos, E Pellegrini Journal of Guidance, Control, and Dynamics 42 (12), 2615-2626, 2019 | 51 | 2019 |
| 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 | 51 | 2004 |
| Jovian tour design for orbiter and lander missions to Europa S Campagnola, BB Buffington, AE Petropoulos Acta Astronautica 100, 68-81, 2014 | 50 | 2014 |
| 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 | 50 | 2009 |
Ryan P. RussellProfessor, Aerospace Engineering, University of Texas at Austin確認したメール アドレス: austin.utexas.edu