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Stefano Campagnola, Ph.D. - Publications

Affiliations: 
2010 Aerospace Engineering University of Southern California, Los Angeles, CA, United States 
Area:
Aerospace Engineering, Applied Mathematics
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46 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2020 Ozaki N, Campagnola S, Funase R. Tube Stochastic Optimal Control for Nonlinear Constrained Trajectory Optimization Problems Journal of Guidance Control and Dynamics. 43: 645-655. DOI: 10.2514/1.G004363  0.375
2020 Funase R, Ikari S, Miyoshi K, Kawabata Y, Nakajima S, Nomura S, Funabiki N, Ishikawa A, Kakihara K, Matsushita S, Takahashi R, Yanagida K, Mori D, Murata Y, Shibukawa T, ... ... Campagnola S, et al. Mission to Earth–Moon Lagrange Point by a 6U CubeSat: EQUULEUS Ieee Aerospace and Electronic Systems Magazine. 35: 30-44. DOI: 10.1109/Maes.2019.2955577  0.433
2020 Oguri K, Oshima K, Campagnola S, Kakihara K, Ozaki N, Baresi N, Kawakatsu Y, Funase R. EQUULEUS Trajectory Design Journal of the Astronautical Sciences. 67: 950-976. DOI: 10.1007/S40295-019-00206-Y  0.506
2019 Campagnola S, Buffington BB, Lam T, Petropoulos AE, Pellegrini E. Tour Design Techniques for the Europa Clipper Mission Journal of Guidance Control and Dynamics. 42: 2615-2626. DOI: 10.2514/1.G004309  0.341
2019 Campagnola S, Hernando-Ayuso J, Kakihara K, Kawabata Y, Chikazawa T, Funase R, Ozaki N, Baresi N, Hashimoto T, Kawakatsu Y, Ikenaga T, Oguri K, Oshima K. Mission Analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI Ieee Aerospace and Electronic Systems Magazine. 34: 38-44. DOI: 10.1109/Maes.2019.2916291  0.448
2019 Hernando-Ayuso J, Campagnola S, Yamaguchi T, Ozawa Y, Ikenaga T. OMOTENASHI trajectory analysis and design: Landing phase Acta Astronautica. 156: 113-124. DOI: 10.1016/J.Actaastro.2018.10.017  0.413
2017 Ozaki N, Campagnola S, Funase R, Yam CH. Stochastic Differential Dynamic Programming with Unscented Transform for Low-Thrust Trajectory Design Journal of Guidance Control and Dynamics. 41: 377-387. DOI: 10.2514/1.G002367  0.371
2017 Tardivel S, Klesh AT, Campagnola S. Technology Enabling Interplanetary Trajectories for Nanospacecraft Journal of Spacecraft and Rockets. 55: 95-105. DOI: 10.2514/1.A33789  0.439
2017 Oshima K, Campagnola S, Yanao T. Global search for low-thrust transfers to the Moon in the planar circular restricted three-body problem Celestial Mechanics and Dynamical Astronomy. 128: 303-322. DOI: 10.1007/S10569-016-9748-2  0.438
2017 Oshima K, Topputo F, Campagnola S, Yanao T. Analysis of medium-energy transfers to the Moon Celestial Mechanics and Dynamical Astronomy. 127: 285-300. DOI: 10.1007/S10569-016-9727-7  0.469
2016 Anderson RL, Campagnola S, Lantoine G. Broad search for unstable resonant orbits in the planar circular restricted three-body problem Celestial Mechanics and Dynamical Astronomy. 124: 177-199. DOI: 10.1007/S10569-015-9659-7  0.457
2015 Lantukh DV, Russell RP, Campagnola S, McLaughlin C. V-infinity leveraging boundary-value problem and application in spacecraft trajectory design Journal of Spacecraft and Rockets. 52: 697-710. DOI: 10.2514/1.A32918  0.454
2015 Campagnola S, Boutonnet A, Martens W, Masters A. Mission design for the exploration of Neptune and Triton Ieee Aerospace and Electronic Systems Magazine. 30: 6-17. DOI: 10.1109/Maes.2015.140119  0.391
2015 Campagnola S, Kawakatsu Y. Design of the Recovery Trajectory for JAXA Venus Orbiter Akatsuki Journal of the Astronautical Sciences. 62: 298-314. DOI: 10.1007/S40295-015-0074-9  0.49
2014 Anderson RL, Campagnola S, Buffngton BB. Analysis of petal rotation trajectory characteristics Aiaa/Aas Astrodynamics Specialist Conference 2014. DOI: 10.2514/1.G002571  0.409
2014 Campagnola S, Boutonnet A, Schoenmaekers J, Grebow DJ, Petropoulos AE, Russell RP. Tisserand-leveraging transfers Journal of Guidance, Control, and Dynamics. 37: 1202-1210. DOI: 10.2514/1.62369  0.441
2014 Masters A, Achilleos N, Agnor CB, Campagnola S, Charnoz S, Christophe B, Coates AJ, Fletcher LN, Jones GH, Lamy L, Marzari F, Nettelmann N, Ruiz J, Ambrosi R, Andre N, et al. Neptune and triton: Essential pieces of the solar system puzzle Planetary and Space Science. 104: 108-121. DOI: 10.1016/J.Pss.2014.05.008  0.325
2014 Campagnola S, Buffington BB, Petropoulos AE. Jovian tour design for orbiter and lander missions to Europa Acta Astronautica. 100: 68-81. DOI: 10.1016/J.Actaastro.2014.02.005  0.463
2014 Giancotti M, Campagnola S, Tsuda Y, Kawaguchi J. Families of periodic orbits in Hill’s problem with solar radiation pressure: application to Hayabusa 2 Celestial Mechanics and Dynamical Astronomy. 120: 269-286. DOI: 10.1007/S10569-014-9564-5  0.421
2014 Yam CH, Sugimoto Y, Ozaki N, Sarli B, Chen H, Campagnola S, Ogura S, Kawabata Y, Kawakatsu Y, Nakajima S, Funase R, Nakasuka S. Launch window and sensitivity analysis of an asteroid flyby mission with miniature ion propulsion system: PROCYON Proceedings of the International Astronautical Congress, Iac. 8: 5383-5389.  0.304
2013 Campagnola S, Kawakatsu Y. Trajectory options for the Akatsuki recovery Proceedings of the International Astronautical Congress, Iac. 7: 5344-5352.  0.42
2013 Sugimoto Y, Kawakatsu Y, Campagnola S, Saiki T. Short and long term closed orbit design in sun-earth Elliptic-Restricted 3-Body Problem Advances in the Astronautical Sciences. 148: 2059-2071.  0.422
2012 Buffington B, Campagnola S, Petropoulos A. Europa multiple-flyby trajectory design Aiaa/Aas Astrodynamics Specialist Conference 2012. DOI: 10.2514/6.2012-5069  0.319
2012 Campagnola S, Kawakatsu Y. Jupiter magnetospheric orbiter: Trajectory design in the jovian system Journal of Spacecraft and Rockets. 49: 318-324. DOI: 10.2514/1.A32055  0.509
2012 Campagnola S, Kawakatsu Y. Three-dimensional resonant hopping strategies and the Jupiter magnetospheric orbiter Journal of Guidance, Control, and Dynamics. 35: 344-349. DOI: 10.2514/1.53334  0.407
2012 Sasaki S, Fujimoto M, Yano H, Takashima T, Kasaba Y, Takahashi Y, Kimura J, Tsuda Y, Funase R, Mori O, Campagnola S, Kawakatsu Y. The Jupiter Magnetospheric Orbiter and the Trojan Asteroid Explorer in EJSM (Europa Jupiter System Mission) Transactions of the Japan Society For Aeronautical and Space Sciences, Space Technology Japan. 10. DOI: 10.2322/Tastj.10.Tk_37  0.424
2012 Campagnola S, Skerritt P, Russell RP. Flybys in the planar, circular, restricted, three-body problem Advances in the Astronautical Sciences. 142: 373-392. DOI: 10.1007/S10569-012-9427-X  0.413
2012 Kawakatsu Y, Campagnola S, Hirose C, Ishii N. An orbit plan toward AKATSUKI Venus reencounter and orbit injection Advances in the Astronautical Sciences. 143: 1535-1547.  0.3
2012 Lantukh DV, Russell RP, Campagnola S. Automated inclusion of v-infinity leveraging maneuvers in gravity-assist flyby tour design Advances in the Astronautical Sciences. 143: 865-884.  0.398
2012 Campagnola S, Skerritt P, Russell RP. Flybys in the planar, circular, restricted, three-body problem Advances in the Astronautical Sciences. 142: 373-392.  0.333
2011 Lantoine G, Russell RP, Campagnola S. Optimization of low-energy resonant hopping transfers between planetary moons Acta Astronautica. 68: 1361-1378. DOI: 10.1016/J.Actaastro.2010.09.021  0.48
2010 Campagnola S, Russell RP. Endgame problem part 2: Multibody technique and the tisserand-poincare graph Journal of Guidance, Control, and Dynamics. 33: 476-486. DOI: 10.2514/1.44290  0.458
2010 Campagnola S, Russell RP. Endgame problem part 1: V∞ -Leveraging technique and the leveraging graph Journal of Guidance, Control, and Dynamics. 33: 463-475. DOI: 10.2514/1.44258  0.453
2010 Campagnola S, Strange NJ, Russell RP. A fast tour design method using non-tangent V-Infinity Leveraging Transfers Advances in the Astronautical Sciences. 136: 983-1003. DOI: 10.1007/S10569-010-9295-1  0.518
2010 Strange NJ, Campagnola S, Russell RP. Leveraging flybys of low mass moons to enable an Enceladus orbiter Advances in the Astronautical Sciences. 135: 2207-2225.  0.384
2009 Gawlik ES, Marsden JE, Du Toit PC, Campagnola S. Lagrangian coherent structures in the planar elliptic restricted three-body problem Celestial Mechanics and Dynamical Astronomy. 103: 227-249. DOI: 10.1007/S10569-008-9180-3  0.384
2009 Campagnola S, Russell RP. The endgame problem part B: The Multi-Body technique and the T-P graph Advances in the Astronautical Sciences. 134: 1905-1924.  0.364
2009 Campagnola S, Russell RP. The Endgame problem part A: V-Infinity Leveraging technique and the Leveraging graph Advances in the Astronautical Sciences. 134: 1867-1886.  0.374
2008 Campagnola S, Lot M, Newton P. Subregions of motion and elliptic halo orbits in the elliptic restricted three-body problem Advances in the Astronautical Sciences. 130: 1541-1555.  0.365
2007 Campagnola S, Lo M. BepiColombo gravitational capture and the elliptic restricted three‐body problem Pamm. 7: 1030905-1030906. DOI: 10.1002/Pamm.200700330  0.474
2005 Campagnola S, Jehn R, Van Damme CC. Design of lunar gravity assist for the bepicolombo mission to mercury Advances in the Astronautical Sciences. 119: 427-441.  0.381
2005 Khan M, Campagnola S, Croon M. End-to-end mission analysis for a low-cost, two-spacecraft mission to Europa Advances in the Astronautical Sciences. 119: 463-471.  0.387
2004 Van Damme CC, Jehn R, Campagnola S. BepiColombo launch window design based on a phasing loop strategy Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference. 3: 1598-1612.  0.386
2004 Jehn R, Campagnola S, Garcia D, Kemble S. Low-thrust approach and gravitational capture at Mercury European Space Agency, (Special Publication) Esa Sp. 487-492.  0.343
2004 D'Amico S, Arbinger C, Kirschner M, Campagnola S. Generation of an optimum target trajectory for the terraSAR-X repeat observation satellite European Space Agency, (Special Publication) Esa Sp. 137-142.  0.359
2003 Pessina SM, Campagnola S, Vasile M. Preliminary analysis of interplanetary trajectories with aerogravity and gravity assist manoeuvres 54th International Astronautical Congress of the International Astronautical Federation (Iaf), the International Academy of Astronautics and the International Institute of Space Law. 1: 671-681.  0.392
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