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Cesar A. Ocampo - Publications

Affiliations: 
Aerospace Engineering University of Texas at Austin, Austin, Texas, U.S.A. 
Area:
Aerospace Engineering
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43 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
2014 Jesick M, Ocampo CA. Automated design of optimal finite thrust orbit insertion with ballistic flyby constraints Journal of Spacecraft and Rockets. 51: 1872-1884. DOI: 10.2514/1.A32886  0.584
2013 Bradley N, Ocampo C. Optimal Free-Return Trajectories to Near-Earth Asteroids Journal of Guidance Control and Dynamics. 36: 1346-1355. DOI: 10.2514/1.59511  0.513
2013 Restrepo RL, Ocampo CA. Automatic algorithm for accurate numerical gradient calculation in general and complex spacecraft trajectories Advances in the Astronautical Sciences. 148: 1433-1448.  0.359
2013 Hernandez S, Akella MR, Ocampo CA. Lyapunov-based elliptical to circular planar orbit transfers in Levi-Civita coordinates Advances in the Astronautical Sciences. 147: 265-279.  0.453
2012 Whitley RJ, Ocampo CA, Williams J. Performance of an autonomous multi-maneuver algorithm for lunar trans-earth injection Journal of Spacecraft and Rockets. 49: 165-174. DOI: 10.2514/1.52710  0.46
2012 Ocampo CA, Mathur R. Variational model for optimization of finite-burn escape trajectories using a direct method Journal of Guidance, Control, and Dynamics. 35: 598-608. DOI: 10.2514/1.52606  0.556
2012 Jones DR, Ocampo C. Optimization of Impulsive Trajectories from a Circular Orbit to an Excess Velocity Vector Journal of Guidance, Control, and Dynamics. 35: 234-244. DOI: 10.2514/1.52527  0.621
2012 Griesemer PR, Ocampo C, Cooley DS. Optimal ballistically captured Earth-Moon transfers Acta Astronautica. 76: 1-12. DOI: 10.1016/J.Actaastro.2012.01.001  0.8
2011 Jesick M, Ocampo C. Optimal Lunar Orbit Insertion from a Variable Symmetric Free-Return Trajectory Journal of Guidance Control and Dynamics. 34: 1867-1875. DOI: 10.2514/1.53826  0.567
2011 Jesick M, Ocampo CA. Automated Generation of Symmetric Lunar Free-Return Trajectories Journal of Guidance Control and Dynamics. 34: 98-106. DOI: 10.2514/1.50550  0.49
2011 Griesemer PR, Ocampo C, Cooley DS. Targeting ballistic lunar capture trajectories using periodic orbits Journal of Guidance, Control, and Dynamics. 34: 893-902. DOI: 10.2514/1.46843  0.777
2011 Jesick M, Ocampo CA. Computation and Optimization of Lunar Orbit Insertion from a Fixed Free Return Journal of the Astronautical Sciences. 58: 35-53. DOI: 10.1007/Bf03321158  0.552
2010 Whitley RJ, Ocampo CA, Williams J. Implementation of an autonomous multi-maneuver targeting sequence for Lunar trans-earth injection Aiaa Guidance, Navigation, and Control Conference. DOI: 10.2514/6.2010-8066  0.316
2010 Ocampo C, Munoz JP. Variational equations for a generalized spacecraft trajectory model Journal of Guidance, Control, and Dynamics. 33: 1615-1622. DOI: 10.2514/1.46953  0.477
2010 Zimmer S, Ocampo C, Bishop R. Reducing Orbit Covariance for Continuous Thrust Spacecraft Transfers Ieee Transactions On Aerospace and Electronic Systems. 46: 771-791. DOI: 10.1109/Taes.2010.5461656  0.8
2010 Jesick MC, Ocampo CA, Condon GL. Lunar orbit insertion from a fixed free return Advances in the Astronautical Sciences. 135: 1225-1244.  0.396
2010 Morcos FM, Ocampo CA. Optimal low-energy transfers in the Concentric Circular Restricted Four-Body Problem Advances in the Astronautical Sciences. 135: 2249-2268.  0.403
2009 Ocampo CA, Saudemont RR. Initial trajectory model for a multi-maneuver moon to Earth abort sequence Advances in the Astronautical Sciences. 134: 1401-1420. DOI: 10.2514/1.46955  0.589
2009 Ranieri CL, Ocampo CA. Indirect optimization of three-dimensional Finite-burning interplanetary transfers including spiral dynamics Journal of Guidance, Control, and Dynamics. 32: 444-454. DOI: 10.2514/1.38170  0.824
2009 Whitley RJ, Ocampo CA. Direct multiple shooting optimization with variable problem parameters 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.  0.533
2009 Jesick MC, Ocampo CA. Automated lunar free return trajectory generation Advances in the Astronautical Sciences. 134: 1371-1388.  0.37
2008 Ranieri CL, Ocampo CA. Indirect optimization of two-dimensional finite burning interplanetary transfers including spiral dynamics Journal of Guidance, Control, and Dynamics. 31: 720-728. DOI: 10.2514/1.30833  0.835
2008 Ranieri CL, Ocampo CA. Indirect optimization of low earth orbit to low lunar orbit transfers Aiaa/Aas Astrodynamics Specialist Conference and Exhibit.  0.837
2007 Ranieri CL, Ocampo CA. Indirect optimization of three dimensional finite-burning interplanetary transfers including spiral dynamics Advances in the Astronautical Sciences. 127: 1565-1584.  0.833
2006 Ranieri CL, Ocampo CA. Indirect optimization of two dimensional finite-burning interplanetary transfers including spiral dynamics Aiaa 57th International Astronautical Congress, Iac 2006. 7: 4838-4850. DOI: 10.2514/1.30833  0.841
2006 Ranieri CL, Ocampo CA. Indirect optimization of spiral trajectories Journal of Guidance, Control, and Dynamics. 29: 1360-1366. DOI: 10.2514/1.19539  0.802
2006 Russell RP, Ocampo CA. Optimization of a broad class of ephemeris model Earth-Mars cyclers Journal of Guidance, Control, and Dynamics. 29: 354-367. DOI: 10.2514/1.13652  0.665
2005 Ocampo CA. Trajectory Analysis for the Lunar Flyby Rescue of AsiaSat-3/HGS-1 Annals of the New York Academy of Sciences. 1065: 232-253. PMID 16510412 DOI: 10.1196/Annals.1370.021  0.443
2005 Zimmer S, Ocampo CA. Analytical Gradients for Gravity Assist Trajectories Using Constant Specific Impulse Engines Journal of Guidance Control and Dynamics. 28: 753-760. DOI: 10.2514/1.9917  0.814
2005 Ranieri CL, Ocampo CA. Optimizing finite-burn, round-trip trajectories with i sp constraints and mass discontinuities Journal of Guidance, Control, and Dynamics. 28: 775-781. DOI: 10.2514/1.9188  0.828
2005 Russell RP, Ocampo CA. Global Search for Idealized Free-Return Earth-Mars Cyclers Journal of Guidance Control and Dynamics. 28: 194-208. DOI: 10.2514/1.8696  0.673
2005 Senent J, Ocampo C, Capella A. Low-Thrust Variable-Specific-Impulse Transfers and Guidance to Unstable Periodic Orbits Journal of Guidance Control and Dynamics. 28: 280-290. DOI: 10.2514/1.6398  0.558
2005 Russell RP, Ocampo CA. Geometric analysis of free-return trajectories following a gravity-assisted flyby Journal of Spacecraft and Rockets. 42: 138-151. DOI: 10.2514/1.5571  0.676
2005 Ranieri CL, Ocampo CA. Optimization of roundtrip, time-constrained, finite burn trajectories via an indirect method Journal of Guidance, Control, and Dynamics. 28: 306-314. DOI: 10.2514/1.5540  0.839
2005 Zimmer S, Ocampo CA. Use of Analytical Gradients to Calculate Optimal Gravity-Assist Trajectories Journal of Guidance Control and Dynamics. 28: 324-332. DOI: 10.2514/1.4825  0.806
2005 Ranieri CL, Ocampo CA. Finite burn, roundtrip interplanetary trajectories with ISP constraints and mass discontinuities Advances in the Astronautical Sciences. 119: 1987-2006.  0.827
2005 Rusself RP, Ocampo CA. Global search for idealized free-return earth-mars cyclers using minimax optimization and combinatorics Advances in the Astronautical Sciences. 119: 679-702.  0.458
2004 Ocampo C. Finite Burn Maneuver Modeling for a Generalized Spacecraft Trajectory Design and Optimization System Annals of the New York Academy of Sciences. 1017: 210-233. PMID 15220149 DOI: 10.1196/Annals.1311.013  0.56
2004 Russell RP, Ocampo CA. Systematic method for constructing earth-mars cyclers using free-return trajectories Journal of Guidance, Control, and Dynamics. 27: 321-335. DOI: 10.2514/1.1011  0.678
2003 Ocampo CA. Transfers to Earth centered orbits via lunar gravity assist Acta Astronautica. 52: 173-179. DOI: 10.1016/S0094-5765(02)00154-6  0.553
2003 Russell RP, Ocampo CA. A systematic method for constructing Earth-Mars cyclers using direct return trajectories Advances in the Astronautical Sciences. 114: 697-716.  0.648
1999 Ocampo CA, Rosborough GW. Multiple-Spacecraft Orbit-Transfer Problem: The No-Booster Case Journal of Guidance, Control, and Dynamics. 22: 650-657. DOI: 10.2514/2.4453  0.572
1999 Ocampo CA, Rosborough GW. Multiple-spacecraft orbit transfer problem: weak-booster and strong-booster cases Journal of Guidance, Control, and Dynamics. 22: 897-904.  0.481
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