| Year |
Citation |
Score |
| 2016 |
Saikia SJ, Rhoads JF, Longuski JM. Improved perturbative solution of yaroshevskii's planetary entry equation Journal of Computational and Nonlinear Dynamics. 11. DOI: 10.1115/1.4033553 |
0.336 |
|
| 2016 |
Martin KM, Landau DF, Longuski JM. Method to maintain artificial gravity during transfer maneuvers for tethered spacecraft Acta Astronautica. 120: 138-153. DOI: 10.1016/J.Actaastro.2015.11.030 |
0.763 |
|
| 2015 |
Hughes KM, Edelman PJ, Saikia SJ, Longuski JM, Loucks ME, Carrico JP, Tito DA. Fast free returns to Mars and Venus with applications to inspiration Mars Journal of Spacecraft and Rockets. 52: 1712-1735. DOI: 10.2514/1.A33293 |
0.43 |
|
| 2015 |
Laipert FE, Longuski JM. Automated missed-thrust propellant margin analysis for low-thrust trajectories Journal of Spacecraft and Rockets. 52: 1135-1143. DOI: 10.2514/1.A33264 |
0.421 |
|
| 2015 |
Martin KM, Longuski JM. Velocity pointing error reduction for spinning, thrusting spacecraft via heuristic thrust profiles Journal of Spacecraft and Rockets. 52: 1268-1272. DOI: 10.2514/1.A33152 |
0.334 |
|
| 2015 |
Rogers BA, Hughes KM, Longuski JM, Aldrin B. Establishing cycler trajectories between Earth and Mars Acta Astronautica. 112: 114-125. DOI: 10.1016/J.Actaastro.2015.03.002 |
0.709 |
|
| 2015 |
Okutsu M, Landau DF, Rogers BA, Longuski JM. Low-thrust roundtrip trajectories to Mars with one-synodic-period repeat time Acta Astronautica. 110: 191-205. DOI: 10.1016/j.actaastro.2015.01.006 |
0.791 |
|
| 2014 |
Henning GA, Edelman PJ, Longuski JM. Design and optimization of interplanetary Aerogravity-Assist Tours Journal of Spacecraft and Rockets. 51: 1849-1856. DOI: 10.2514/1.A32881 |
0.443 |
|
| 2014 |
Ayoubi MA, Martin KM, Longuski JM. Analytical solution for spinning thrusting spacecraft with transverse Ramp-Up torques Journal of Guidance, Control, and Dynamics. 37: 1272-1282. DOI: 10.2514/1.62695 |
0.729 |
|
| 2014 |
Rogers BA, Longuski JM. Preliminary analysis of establishing cycler trajectories between earth and mars via low thrust Advances in the Astronautical Sciences. 150: 1555-1563. |
0.631 |
|
| 2014 |
Laipert FE, Longuski JM. Automated missed-thrust propellant margin analysis for low-thrust missions to mars and a near-earth asteroid Aiaa/Aas Astrodynamics Specialist Conference 2014. |
0.307 |
|
| 2014 |
Rogers BA, Longuski JM, Fischbach E. A proposed mission to detect solar influences on nuclear decay rates Advances in the Astronautical Sciences. 150: 1605-1616. |
0.542 |
|
| 2014 |
Strange NJ, Landau DF, Longuski JM. Design of initial inclination reduction sequence for uranian gravity-assist tours Advances in the Astronautical Sciences. 150: 1469-1485. |
0.78 |
|
| 2014 |
Laipert FE, Longuski JM, Minton DA. Preliminary sample return mission design for asteroid (216) Kleopatra Advances in the Astronautical Sciences. 150: 3273-3280. |
0.305 |
|
| 2014 |
Hughes KM, Moore JW, Longuski JM. Preliminary analysis of ballistic trajectories to neptune via gravity assists from venus, earth, mars, jupiter, saturn, and uranus Advances in the Astronautical Sciences. 150: 1535-1554. |
0.329 |
|
| 2014 |
Edelman PJ, Hughes KM, Longuski JM, Loucks ME, Carrico JP, Tito DA. Inspiration mars 2018 free-return opportunity Aiaa/Aas Astrodynamics Specialist Conference 2014. |
0.354 |
|
| 2012 |
Ayoubi MA, Martin KM, Longuski JM. Analytical solution of the motion of spinning thrusting spacecraft with transverse ramp-up torques Aiaa/Aas Astrodynamics Specialist Conference 2012. DOI: 10.2514/6.2012-5015 |
0.705 |
|
| 2012 |
Rogers BA, Hughes KM, Longuski JM, Aldrin B. Preliminary analysis of establishing cycler trajectories between earth and mars via V∞ leveraging Aiaa/Aas Astrodynamics Specialist Conference 2012. DOI: 10.2514/6.2012-4746 |
0.662 |
|
| 2012 |
Mueterthies MJ, Longuski JM. Modeling and analysis of the electrodynamic tether sling Aiaa/Aas Astrodynamics Specialist Conference 2012. DOI: 10.2514/6.2012-4660 |
0.32 |
|
| 2012 |
Joseph Chen K, Rogers BA, Okutsu M, Landau DF, Longuski JM. Low-thrust aldrin cycler with reduced encounter velocities Journal of Spacecraft and Rockets. 49: 955-961. DOI: 10.2514/1.A32109 |
0.821 |
|
| 2012 |
Krause DE, Rogers BA, Fischbach E, Buncher JB, Ging A, Jenkins JH, Longuski JM, Strange N, Sturrock PA. Searches for solar-influenced radioactive decay anomalies using spacecraft RTGs Astroparticle Physics. 36: 51-56. DOI: 10.1016/J.Astropartphys.2012.05.002 |
0.631 |
|
| 2012 |
Laipert FE, Longuski JM. Low-thrust trajectories for human missions to ceres Aiaa/Aas Astrodynamics Specialist Conference 2012. DOI: 10.1016/J.Actaastro.2013.11.003 |
0.443 |
|
| 2012 |
Okutsu M, Yam CH, Longuski JM, Strange NJ. Cassini Saturn-escape trajectories to Jupiter, Uranus, and Neptune Acta Astronautica. 79: 157-167. DOI: 10.1016/J.Actaastro.2012.04.034 |
0.822 |
|
| 2012 |
Lynam AE, Longuski JM. Preliminary analysis for the navigation of multiple-satellite-aided capture sequences at Jupiter Advances in the Astronautical Sciences. 142: 2003-2022. DOI: 10.1016/J.Actaastro.2012.04.012 |
0.802 |
|
| 2012 |
Lynam AE, Longuski JM. Preliminary analysis for the navigation of multiple-satellite-aided capture sequences at Jupiter Advances in the Astronautical Sciences. 142: 2003-2022. DOI: 10.1016/j.actaastro.2012.04.012 |
0.792 |
|
| 2012 |
Fischbach E, Chen KJ, Gold RE, Goldsten JO, Lawrence DJ, McNutt RJ, Rhodes EA, Jenkins JH, Longuski J. Solar influence on nuclear decay rates: Constraints from the MESSENGER mission Astrophysics and Space Science. 337: 39-45. DOI: 10.1007/S10509-011-0808-5 |
0.336 |
|
| 2012 |
Spreen CM, Mueterthies MJ, Kloster KW, Longuski JM. Preliminary analysis of ballistic trajectories to Uranus using gravity-assists from Venus, Earth, Mars, Jupiter, and Saturn Advances in the Astronautical Sciences. 142: 3411-3428. |
0.811 |
|
| 2012 |
Ayoubi MA, Landau D, Longuski JM. Solution of spacecraft attitude via angular momentum in body and inertial frames Advances in the Astronautical Sciences. 142: 2611-2628. |
0.699 |
|
| 2011 |
Lynam AE, Longuski JM. Interplanetary trajectories for multiple satellite-aided capture at Jupiter Journal of Guidance, Control, and Dynamics. 34: 1485-1494. DOI: 10.2514/1.53251 |
0.822 |
|
| 2011 |
Lynam AE, Longuski JM. Laplace-resonant triple-cyclers for missions to Jupiter Acta Astronautica. 69: 158-167. DOI: 10.1016/J.Actaastro.2011.03.011 |
0.783 |
|
| 2011 |
Kloster KW, Petropoulos AE, Longuski JM. Europa orbiter tour design with Io gravity assists Acta Astronautica. 68: 931-946. DOI: 10.1016/J.Actaastro.2010.08.041 |
0.814 |
|
| 2011 |
Pollock GE, Gangestad JW, Longuski JM. Analytical solutions for the relative motion of spacecraft subject to Lorentz-force perturbations Acta Astronautica. 68: 204-217. DOI: 10.1016/J.Actaastro.2010.07.007 |
0.819 |
|
| 2011 |
Lynam AE, Kloster KW, Longuski JM. Multiple-satellite-aided capture trajectories at Jupiter using the Laplace resonance Celestial Mechanics and Dynamical Astronomy. 109: 59-84. DOI: 10.1007/S10569-010-9307-1 |
0.801 |
|
| 2010 |
Pollock GE, Gangestad JW, Longuski JM. Inclination change in low-earth orbit via the geomagnetic lorentz force Journal of Guidance, Control, and Dynamics. 33: 1387-1395. DOI: 10.2514/1.48610 |
0.813 |
|
| 2010 |
Gangestad JW, Pollock GE, Longuski JM. Analytical expressions that characterize propellantless capture with electrostatically charged spacecraft Advances in the Astronautical Sciences. 136: 489-508. DOI: 10.2514/1.47849 |
0.807 |
|
| 2010 |
Gangestad JW, Pollock GE, Longuski JM. Analytical expressions that characterize propellantless capture with electrostatically charged spacecraft Advances in the Astronautical Sciences. 136: 489-508. DOI: 10.2514/1.47849 |
0.808 |
|
| 2010 |
Gates KL, Longuski JM. Aerocapture ballutes versus aerocapture tethers for exploration of the solar system Journal of Spacecraft and Rockets. 47: 590-596. DOI: 10.2514/1.46603 |
0.42 |
|
| 2010 |
Gangestad JW, Pollock GE, Longuski JM. Lagrange's planetary equations for the motion of electrostatically charged spacecraft Celestial Mechanics and Dynamical Astronomy. 108: 125-145. DOI: 10.1007/S10569-010-9297-Z |
0.813 |
|
| 2010 |
Pollock GE, Gangestad JW, Longuski JM. Lorentz augmentation of gravity-assist flybys with electrostatically charged spacecraft Advances in the Astronautical Sciences. 136: 1881-1899. |
0.808 |
|
| 2010 |
Gangestad JW, Pollock GE, Longuski JM. Constraints on the motion of electrostatically charged spacecraft Advances in the Astronautical Sciences. 135: 657-674. |
0.817 |
|
| 2010 |
Pollock GE, Gangestad JW, Longuski JM. Charged spacecraft formations: A trade study on Coulomb and Lorentz forces Advances in the Astronautical Sciences. 135: 1439-1458. |
0.797 |
|
| 2010 |
Lynam AE, Kloster KW, Longuski JM. An assessment of multiple satellite-aided capture at Jupiter Advances in the Astronautical Sciences. 135: 2031-2056. |
0.813 |
|
| 2010 |
Kloster KW, Petropoulos AE, Longuski JM. Europa Orbiter mission design with Io gravity assists Advances in the Astronautical Sciences. 135: 875-889. |
0.802 |
|
| 2010 |
Pollock GE, Gangestad JW, Longuski JM. Propellantless formation flight via Coulomb and Lorentz forces Jbis - Journal of the British Interplanetary Society. 63: 2-8. |
0.797 |
|
| 2009 |
Kloster KW, Yam CH, Longuski JM. Saturn escape options for Cassini encore missions Journal of Spacecraft and Rockets. 46: 874-882. DOI: 10.2514/1.42893 |
0.799 |
|
| 2009 |
Gangestad JW, Pollock GE, Longuski JM. Propellantless stationkeeping at enceladus via the electromagnetic Lorentz force Journal of Guidance, Control, and Dynamics. 32: 1466-1475. DOI: 10.2514/1.42769 |
0.806 |
|
| 2009 |
Yam CH, Davis DC, Longuski JM, Howell KC, Buffington B. Saturn impact trajectories for cassini end-of-mission Journal of Spacecraft and Rockets. 46: 353-364. DOI: 10.2514/1.38760 |
0.735 |
|
| 2009 |
Landau DF, Longuski JM. Comparative assessment of human-Mars-mission technologies and architectures Acta Astronautica. 65: 893-911. DOI: 10.1016/J.Actaastro.2009.02.008 |
0.771 |
|
| 2009 |
Ayoubi MA, Longuski JM. Asymptotic theory for thrusting, spinning-up spacecraft maneuvers Acta Astronautica. 64: 810-831. DOI: 10.1016/J.Actaastro.2008.12.015 |
0.741 |
|
| 2008 |
Kloster KW, Hong Yam C, Longuski JM. Saturn escape options for Cassini encore missions Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. DOI: 10.2514/1.42893 |
0.803 |
|
| 2008 |
Ayoubi MA, Longuski JM. Asymptotic theory and limiting cases for spinning spacecraft subject to constant forces Q Journal of Guidance, Control, and Dynamics. 31: 1511-1515. DOI: 10.2514/1.35602 |
0.712 |
|
| 2008 |
Ayoubi MA, Longuski JM. Analytical solutions for translational motion of spinning-up rigid bodies subject to constant body-fixed forces and moments Journal of Applied Mechanics, Transactions Asme. 75: 0110041-0110048. DOI: 10.1115/1.2755110 |
0.723 |
|
| 2008 |
Okutsu M, Yam CH, Longuski JM, Strange NJ. Cassini end-of-life escape trajectories to the outer planets Advances in the Astronautical Sciences. 129: 117-143. |
0.786 |
|
| 2008 |
Gangestad JW, Pollock GE, Longuski JM. The dynamics of Lorentz spacecraft with application to a mission to Enceladus Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.803 |
|
| 2008 |
Chen KJ, Kloster KW, Longuski JM. A graphical method for preliminary design of low-thrust gravity-assist trajectories Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.796 |
|
| 2008 |
Pollock GE, Gangestad JW, Longuski JM. Analysis of Lorentz spacecraft motion about Earth using the Hill-Clohessy-Wiltshire equations Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.816 |
|
| 2008 |
Patterson C, Kakoi M, Howell KC, Yam CH, Longuski JM. 500-Year eccentric orbits for the cassini spacecraft within the saturn system Advances in the Astronautical Sciences. 129: 77-92. |
0.714 |
|
| 2008 |
Yam CH, Davis DC, Longuski JM, Howell KC. Saturn impact trajectories for cassini end-of-life Advances in the Astronautical Sciences. 129: 93-116. |
0.625 |
|
| 2007 |
Ayoubi MA, Longuski JM. Axial velocity solution for spinning-up rigid bodies subject to constant forces Journal of Guidance, Control, and Dynamics. 30: 1610-1618. DOI: 10.2514/1.29617 |
0.726 |
|
| 2007 |
Landau DF, Longuski JM. Human exploration of mars via earth-mars semicyclers Journal of Spacecraft and Rockets. 44: 203-210. DOI: 10.2514/1.23189 |
0.804 |
|
| 2006 |
Chen KJ, Okutsu M, Landau DF, Longuski JM. Low-thrust aldrin cycler with reduced encounter velocities Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 1: 112-121. DOI: 10.2514/1.A32109 |
0.819 |
|
| 2006 |
Landau DF, Longuski JM. Guidance strategy for hyperbolic rendezvous Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 2: 753-768. DOI: 10.2514/1.30071 |
0.772 |
|
| 2006 |
Landau DF, Longuski JM. Trajectories for human missions to mars, part 2: Low-thrust transfers Journal of Spacecraft and Rockets. 43: 1043-1047. DOI: 10.2514/1.21954 |
0.791 |
|
| 2006 |
Landau DF, Longuski JM. Trajectories for human missions to Mars, part 1: Impulsive transfers Journal of Spacecraft and Rockets. 43: 1035-1042. DOI: 10.2514/1.18995 |
0.799 |
|
| 2006 |
McConaghy TT, Landau DF, Yam CH, Longuski JM. Notable two-synodic-period earth-mars cycler Journal of Spacecraft and Rockets. 43: 456-465. DOI: 10.2514/1.15215 |
0.814 |
|
| 2006 |
Okutsu M, Landauf DF, Longuski JM. Low-thrust roundtrip trajectories to Mars with one-synodic-period repeat time Advances in the Astronautical Sciences. 123: 2285-2300. DOI: 10.1016/J.Actaastro.2015.01.006 |
0.708 |
|
| 2006 |
Yam CH, Longuski JM. Reduced parameterization for optimization of low-thrust gravity-assist trajectories: Case studies Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 3: 1842-1857. |
0.713 |
|
| 2006 |
Ayoubi MA, Longuski JM. Transverse velocity solution for a spinning-up rigid body subject to constant body-fixed forces and moments Advances in the Astronautical Sciences. 123: 183-197. |
0.698 |
|
| 2006 |
Ayoubi MA, Longuski JM. Axial velocity solution for a spinning-up rigid body subject to constant body-fixed forces and moments Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 2: 1468-1479. |
0.7 |
|
| 2006 |
Landau DF, Longuski JM. Mars exploration via Earth-Mars semi-cyclers Advances in the Astronautical Sciences. 123: 307-323. |
0.794 |
|
| 2006 |
Yam CH, Longuski JM. Optimization of low-thrust gravity-assist trajectories with a reduced parameterization of the thrust vector Advances in the Astronautical Sciences. 123: 1929-1948. |
0.68 |
|
| 2006 |
Okutsu M, Yam CH, Longuski JM. Low-thrust trajectories to Jupiter via gravity assists from Venus, Earth, and Mars Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 3: 1858-1871. |
0.796 |
|
| 2006 |
Landau DF, Longuski JM, Aldrin B. Continuous Mars habitation with a limited number of cycler vehicles Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 1: 99-111. |
0.759 |
|
| 2006 |
Medlock KLG, Ayoubi MA, Longuski JM, Lyons DT. Analytic solutions for aerocapture, descent, and landing trajectories for dual-use ballute systems Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference, 2006. 1: 147-171. |
0.691 |
|
| 2005 |
McConaghy TT, Russell RP, Longuski JM. Toward a standard nomenclature for Earth-Mars cycler trajectories Journal of Spacecraft and Rockets. 42: 694-698. DOI: 10.2514/1.8123 |
0.813 |
|
| 2005 |
Park RS, Scheeres DJ, Giampieri G, Longuski JM, Fischbach E. Estimating parameterized post-Newtonian parameters from spacecraft radiometric tracking data Journal of Spacecraft and Rockets. 42: 559-568. DOI: 10.2514/1.7647 |
0.54 |
|
| 2005 |
Landau DF, Longuski JM, Penzo PA. Method for parking-orbit reorientation for human missions to Mars Journal of Spacecraft and Rockets. 42: 517-522. DOI: 10.2514/1.7042 |
0.802 |
|
| 2005 |
Jokic MD, Longuski JM. Artificial gravity and abort scenarios via tethers for human missions to mars Journal of Spacecraft and Rockets. 42: 883-889. DOI: 10.2514/1.6121 |
0.499 |
|
| 2005 |
Longuski JM, Gick RA, Ayoubi MA, Randall L. Analytical solutions for thrusting, spinning spacecraft subject to constant forces Journal of Guidance, Control, and Dynamics. 28: 1301-1308. DOI: 10.2514/1.12272 |
0.721 |
|
| 2005 |
Chen KJ, McConaghy TT, Landau DF, Longuski JM, Aldrin B. Powered earth-mars cycler with three-synodic-period repeat time Journal of Spacecraft and Rockets. 42: 921-927. DOI: 10.2514/1.11610 |
0.803 |
|
| 2004 |
Petropoulos AE, Longuski JM. Shape-based algorithm for automated design of low-thrust, gravity-assist trajectories Journal of Spacecraft and Rockets. 41: 787-796. DOI: 10.2514/1.13095 |
0.755 |
|
| 2004 |
Johnson WR, Longuski JM, Lyons DT. Six-degree-of-freedom modeling of semi-autonomous attitude control during aerobraking Journal of Spacecraft and Rockets. 41: 797-804. DOI: 10.2514/1.13078 |
0.585 |
|
| 2004 |
Longuski JM, Fischbach E, Scheeres DJ, Giampieri G, Park RS. Deflection of spacecraft trajectories as a new test of general relativity: Determining then parametrized post-Newtonian parameters β and γ Physical Review D. 69. DOI: 10.1103/Physrevd.69.042001 |
0.525 |
|
| 2004 |
Park RS, Fischbach E, Giampieri G, Longuski JM, Scheeres DJ. A test of general relativity: Estimating PPN parameters γ and β from spacecraft radiometric tracking data Nuclear Physics B - Proceedings Supplements. 134: 181-183. DOI: 10.1016/j.nuclphysbps.2004.08.028 |
0.452 |
|
| 2004 |
McConaghy TT, Longuski JM. Parameterization effects on convergence when optimizing a low-thrust trajectory with gravity assists Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference. 3: 1668-1687. |
0.805 |
|
| 2004 |
Landau DF, Longuski JM. A reassessment of trajectory options for human missions to Mars Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference. 2: 836-871. |
0.789 |
|
| 2004 |
Yam CH, McConaghy TT, Chen KJ, Longuski JM. Preliminary design of nuclear electric propulsion missions to the outer planets Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference. 3: 1542-1561. |
0.825 |
|
| 2004 |
McConaghy TT, Longuski JM, Byrnes DV. Analysis of a class of earth-mars cycler trajectories Journal of Spacecraft and Rockets. 41: 622-628. |
0.817 |
|
| 2004 |
Yam CH, McConaghy TT, Chen KJ, Longuski JM. Design of low-thrust gravity-assist trajectories to the outer planets International Astronautical Federation - 55th International Astronautical Congress 2004. 1: 476-491. |
0.827 |
|
| 2004 |
Park RS, Scheeres DJ, Giampieri G, Longuski JM, Fischbach E. Orbit design for general relativity experiments: Heliocentric and mercury-centric cases Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference. 3: 1562-1577. |
0.484 |
|
| 2003 |
Johnson WR, Longuski JM, Lyons DT. Nondimensional Analysis of Reaction-Wheel Control for Aerobraking Journal of Guidance, Control, and Dynamics. 26: 861-868. DOI: 10.2514/2.6930 |
0.567 |
|
| 2003 |
McConaghy TT, Debban TJ, Petropoulos AE, Longuski JM. Design and optimization of low-thrust trajectories with gravity assists Journal of Spacecraft and Rockets. 40: 380-387. DOI: 10.2514/2.3973 |
0.819 |
|
| 2003 |
Johnson WR, Longuski JM, Lyons DT. Pitch control during autonomous aerobraking for near-term Mars exploration Journal of Spacecraft and Rockets. 40: 371-379. DOI: 10.2514/2.3972 |
0.594 |
|
| 2003 |
Heaton AF, Longuski JM. Feasibility of a Galileo-style tour of the Uranian satellites Journal of Spacecraft and Rockets. 40: 591-596. |
0.399 |
|
| 2002 |
Heaton AF, Strange NJ, Longuski JM, Bonfiglio EP. Automated design of the Europa Orbiter tour Journal of Spacecraft and Rockets. 39: 17-22. DOI: 10.2514/2.3801 |
0.476 |
|
| 2002 |
Strange NJ, Longuski JM. Graphical method for gravity-assist trajectory design Journal of Spacecraft and Rockets. 39: 9-16. DOI: 10.2514/2.3800 |
0.411 |
|
| 2002 |
Okutsu M, Longuski JM. Mars free returns via gravity assist from Venus Journal of Spacecraft and Rockets. 39: 31-36. DOI: 10.2514/2.3778 |
0.738 |
|
| 2002 |
Jokic MD, Longuski JM. Design of a tether sling for human transportation systems between earth and mars Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. DOI: 10.2514/1.2413 |
0.374 |
|
| 2002 |
Okutsu M, Longuski JM. Mars free returns via gravity assist from Venus Journal of Spacecraft and Rockets. 39: 31-36. |
0.715 |
|
| 2002 |
Heaton AF, Longuski JM. The feasibility of a Galileo-style tour of the Uranian satellites Advances in the Astronautical Sciences. 109: 2285-2296. |
0.347 |
|
| 2002 |
Petropoulos AE, Longuski JM. A shape-based algorithm for the automated design of low-thrust, gravity-assist trajectories Advances in the Astronautical Sciences. 109: 2321-2336. |
0.741 |
|
| 2002 |
Johnson WR, Longuski JM. Design of aerogravity-assist trajectories Journal of Spacecraft and Rockets. 39: 23-30. |
0.613 |
|
| 2002 |
Okutsu M, Debban TJ, Longuski JM. Tour design strategies for the Europa Orbiter mission Advances in the Astronautical Sciences. 109: 2269-2284. |
0.71 |
|
| 2002 |
Chen KJ, Mcconaghy TT, Okutsu M, Longuski JM. A low-thrust version of the Aldrin cycler Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.801 |
|
| 2002 |
Debban TJ, Troy McConaghy T, Longuski JM. Design and optimization of low-thrust gravity-assist trajectories to selected planets Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.331 |
|
| 2002 |
Mcconaghy TT, Longuski JM, Byrnes DV. Analysis of a broad class of earth-mars cycler trajectories Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.79 |
|
| 2002 |
Troy McConaghy T, Debban TJ, Petropoulos AE, Longuski JM. An approach to design and optimization of low-thrust trajectories with gravity assists Advances in the Astronautical Sciences. 109: 2337-2355. |
0.713 |
|
| 2002 |
Byrnes DV, Mcconaghy TT, Longuski JM. Analysis of various two synodic period Earth-Mars cycler trajectories Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.811 |
|
| 2002 |
Chen KJ, Landau DF, Mcconaghy TT, Okutsu M, Longuski JM, Aldrin B. Preliminary analysis and design of powered earth-mars cycling trajectories Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.779 |
|
| 2001 |
Longuski JM, Fischbach E, Scheeres DJ. Deflection of spacecraft trajectories as a new test of general relativity Physical Review Letters. 86: 2942-2945. PMID 11290078 DOI: 10.1103/Physrevlett.86.2942 |
0.562 |
|
| 2000 |
Gick RA, Williams MH, Longuski JM. Periodic solutions for spinning asymmetric rigid bodies with constant principal-axis torque Journal of Guidance, Control, and Dynamics. 23: 781-788. DOI: 10.2514/2.4633 |
0.396 |
|
| 2000 |
Johnson WR, Longuski JM. Design of aerogravity-assist trajectories Astrodynamics Specialist Conference. 146-156. DOI: 10.2514/2.3802 |
0.628 |
|
| 2000 |
Bonfiglio EP, Longuski JM, Vinh NX. Automated design of aerogravity-assist trajectories Advances in the Astronautical Sciences. 103: 909-928. DOI: 10.2514/2.3649 |
0.649 |
|
| 2000 |
Javorsek D, Longuski JM. Velocity pointing errors associated with spinning thrusting spacecraft Advances in the Astronautical Sciences. 103: 2347-2364. DOI: 10.2514/2.3586 |
0.38 |
|
| 2000 |
Sims JA, Longuski JM, Patel MR. Aerogravity-assist trajectories to the outer planets and the effect of drag Journal of Spacecraft and Rockets. 37: 49-55. DOI: 10.2514/2.3525 |
0.474 |
|
| 2000 |
Petropoulos AE, Longuski JM. Automated design of low-thrust gravity-assist trajectories Astrodynamics Specialist Conference. 157-166. |
0.732 |
|
| 2000 |
Vinh NX, Johrisor WR, Longuski JM. Mars aerocapture using bank modulation Astrodynamics Specialist Conference. 497-506. |
0.617 |
|
| 2000 |
Petropoulos AE, Longuski JM, Vinh NX. Shape-based analytic representations of low-thrust trajectories for gravity-assist applications Advances in the Astronautical Sciences. 103: 563-581. |
0.787 |
|
| 1999 |
Anne Gick R, Williams MH, Longuski JM. Floquet Approximation for a Nearly Axisymmetric Rigid Body with Constant Transverse Torque Journal of Guidance, Control, and Dynamics. 22: 658-663. DOI: 10.2514/2.4454 |
0.364 |
|
| 1999 |
Longuski JM, Tragesser SG, Puig-Suari J. Characterization of the optimal mass problem for aerobraking tethers Acta Astronautica. 44: 227-241. DOI: 10.1016/S0094-5765(99)00021-1 |
0.444 |
|
| 1999 |
Tragesser SG, Longuski JM. Modeling issues concerning motion of the Saturnian satellites Journal of the Astronautical Sciences. 47: 275-294. DOI: 10.1007/Bf03546204 |
0.424 |
|
| 1998 |
Biswell BL, Puig-Suari J, Longuski JM, Tragesser SG. Three-dimensional hinged-rod model for elastic aerobraking tethers Journal of Guidance, Control, and Dynamics. 21: 286-295. DOI: 10.2514/2.4234 |
0.429 |
|
| 1998 |
Petropoulos AE, Longuski JM, Bonfiglio EP. Trajectories to Jupiter via Gravity assists from Venus, Earth, and Mars Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. 116-126. DOI: 10.2514/2.3650 |
0.753 |
|
| 1998 |
Tragesser SG, Longuski JM. Analysis and design of aerocapture tether with accounting for stochastic errors Journal of Spacecraft and Rockets. 35: 683-689. DOI: 10.2514/2.3385 |
0.392 |
|
| 1998 |
Patel MR, Longuski JM, Sims JA. Mars free return trajectories Journal of Spacecraft and Rockets. 35: 350-354. DOI: 10.2514/2.3333 |
0.394 |
|
| 1998 |
Petropoulos AE, Longuski JM, Bonfiglio EP. Trajectories to Jupiter via Gravity assists from Venus, Earth, and Mars Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. 116-126. |
0.735 |
|
| 1997 |
Tragesser SG, Longuski JM, Puig-Suari J. Global Minimum Mass for Aerobraking Tethers Journal of Guidance, Control, and Dynamics. 20: 1260-1263. DOI: 10.2514/2.7598 |
0.455 |
|
| 1997 |
Sims JA, Longuski JM, Staugler AJ. V∞ leveraging for interplanetary missions: Multiple-revolution orbit techniques Journal of Guidance, Control, and Dynamics. 20: 409-415. DOI: 10.2514/2.4064 |
0.46 |
|
| 1997 |
Sims JA, Staugler AJ, Longuski JM. Trajectory options to Pluto via gravity assists from Venus, Mars, and Jupiter Journal of Spacecraft and Rockets. 34: 347-353. DOI: 10.2514/2.3215 |
0.472 |
|
| 1997 |
Sims JA, Longuski JM, Staugler AJ. Trajectory options for low-cost missions to asteroids Acta Astronautica. 41: 731-737. DOI: 10.1016/S0094-5765(98)00003-4 |
0.416 |
|
| 1996 |
Tsiotras P, Longuski JM. Analytic solution of Euler's equations of motion for an asymmetric rigid body Journal of Applied Mechanics, Transactions Asme. 63: 149-155. DOI: 10.1115/1.2787190 |
0.582 |
|
| 1996 |
Tsiotras P, Longuski JM. Comments on a new parameterization of the attitude kinematics Astrodynamics Conference. 514-522. |
0.506 |
|
| 1995 |
Longuski JM, Puig-Suari J, Tsiotras P, Tragesser S. Optimal mass for aerobraking tethers Acta Astronautica. 35: 489-500. DOI: 10.1016/0094-5765(95)00006-L |
0.655 |
|
| 1995 |
Longuski JM, Puig-Suari J, Mechalas J. Aerobraking tethers for the exploration of the solar system Acta Astronautica. 35: 205-214. DOI: 10.1016/0094-5765(94)00273-O |
0.446 |
|
| 1995 |
Puig-Suari J, Longuski JM, Tragesser SG. A tether sling for lunar and interplanetary exploration Acta Astronautica. 36: 291-295. DOI: 10.1016/0094-5765(94)00235-E |
0.422 |
|
| 1995 |
Sims JA, Longuski JM, Patel MR. Aerogravity-assist trajectories to the outer planets Acta Astronautica. 35: 297-306. DOI: 10.1016/0094-5765(94)00195-R |
0.444 |
|
| 1995 |
Patel MR, Longuski JM, Sims JA. A Uranus—Neptune—Pluto opportunity Acta Astronautica. 35: 287-296. DOI: 10.1016/0094-5765(94)00194-Q |
0.384 |
|
| 1995 |
Tsiotras P, Corless M, Longuski JM. A novel approach to the attitude control of axisymmetric spacecraft Automatica. 31: 1099-1112. DOI: 10.1016/0005-1098(95)00010-T |
0.564 |
|
| 1994 |
Tsiotras P, Longuski JM. Spin-axis stabilization of symmetric spacecraft with two control torques Systems and Control Letters. 23: 395-402. DOI: 10.1016/0167-6911(94)90093-0 |
0.559 |
|
| 1994 |
Tsiotras P, Longuski JM. New kinematic relations for the large angle problem in rigid body attitude dynamics Acta Astronautica. 32: 181-190. DOI: 10.1016/0094-5765(94)90051-5 |
0.581 |
|
| 1994 |
Petropoulos AE, Longuski JM. Analysis of mapping coverage obtained from spacecraft Celestial Mechanics &Amp; Dynamical Astronomy. 60: 431-454. DOI: 10.1007/Bf00692027 |
0.688 |
|
| 1993 |
Byrnes DV, Longuski JM, Aldrin B. Cycler orbit between Earth and Mars Journal of Spacecraft and Rockets. 30: 334-336. DOI: 10.2514/3.25519 |
0.477 |
|
| 1993 |
Tsiotras P, Longuski JM. Analytic solutions for a spinning rigid body subject to time-varying body fixed torques, Part II: Time-varying axial torque Journal of Applied Mechanics, Transactions Asme. 60: 976-981. DOI: 10.1115/1.2901011 |
0.576 |
|
| 1993 |
Longuski JM, Tsiotras P. Analytical solutions for a spinning rigid body subject to time-varying body-fixed torques, Part I: Constant axial torque Journal of Applied Mechanics, Transactions Asme. 60: 970-975. |
0.543 |
|
| 1993 |
Tsiotras P, Corless M, Longuski JM. Invariant manifold techniques for attitude control of symmetric spacecraft Proceedings of the Ieee Conference On Decision and Control. 2: 1470-1475. |
0.509 |
|
| 1992 |
Longuski JM, Todd RE, Konig WW. Survey of nongravitational forces and space environmental torques - Applied to the Galileo Journal of Guidance, Control, and Dynamics. 15: 545-553. DOI: 10.2514/3.20874 |
0.373 |
|
| 1992 |
Longuski JM. Probabilities of escape, re-entry, and orbit decay due to misdirected injection maneuvers Journal of Guidance, Control, and Dynamics. 15: 410-415. DOI: 10.2514/3.20851 |
0.403 |
|
| 1992 |
Ostoja-Starzewski M, Longuski JM. Stochastic Hill's equations for the study of errant rocket burns in orbit Celestial Mechanics and Dynamical Astronomy. 54: 295-303. DOI: 10.1007/Bf00049143 |
0.346 |
|
| 1992 |
Tsiotras P, Longuski JM. Analytic solutions for the attitude motion of spinning rigid bodies subject to periodic torques Advances in the Astronautical Sciences. 76: 661-678. |
0.546 |
|
| 1992 |
Longuski JM, Tsiotras P. Attitude motion of a rigid body subject to polynomial torques Advances in the Astronautical Sciences. 76: 679-690. |
0.534 |
|
| 1991 |
Williams SN, Longuski JM. Low energy trajectories to Mars via gravity assist from Venus to Earth Journal of Spacecraft and Rockets. 28: 486-494. DOI: 10.2514/3.26270 |
0.411 |
|
| 1991 |
Longuski JM. Real solutions for the attitude motion of a self-excited rigid body Acta Astronautica. 25: 131-139. DOI: 10.1016/0094-5765(91)90140-Z |
0.371 |
|
| 1991 |
Puig-Suari J, Longuski JM. Modeling and analysis of orbiting tethers in an atmosphere Acta Astronautica. 25: 679-686. DOI: 10.1016/0094-5765(91)90044-6 |
0.422 |
|
| 1991 |
Tsiotras P, Longuski JM. A complex analytic solution for the attitude motion of a near-symmetric rigid body under body-fixed torques Celestial Mechanics and Dynamical Astronomy. 51: 281-301. DOI: 10.1007/Bf00051695 |
0.573 |
|
| 1991 |
Longuski JM, Williams SN. Automated design of gravity-assist trajectories to Mars and the outer planets Celestial Mechanics and Dynamical Astronomy. 52: 207-220. DOI: 10.1007/Bf00048484 |
0.458 |
|
| 1985 |
Hintz GR, Longuski JM. Error analyses for the delivery of a spinning probe to Jupiter Journal of Guidance, Control, and Dynamics. 8: 384-390. DOI: 10.2514/3.19991 |
0.326 |
|
| 1984 |
Longuski JM, Kia T. A parametric study of the behavior of the angular momentum vector during spin rate changes of rigid-body spacecraft Journal of Guidance, Control, and Dynamics. 7: 295-300. DOI: 10.2514/3.19858 |
0.362 |
|
| 1979 |
Vinh NX, Longuski JM, Busemann A, Culp RD. Analytic theory of orbit contraction due to atmospheric drag Acta Astronautica. 6: 697-723. DOI: 10.1016/0094-5765(79)90028-6 |
0.772 |
|
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