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Solar Sail Capabilities to Reach Elliptic Rectilinear OrbitsQUARTA, Alessandro A; MENGALI, Giovanni.Journal of guidance, control, and dynamics. 2011, Vol 34, Num 3, pp 923-927, issn 0731-5090, 5 p.Article
Orbital Targeting Using Reduced Eccentric Anomaly Low-Thrust CoefficientsHUDSON, Jennifer S; SCHEERES, Daniel J.Journal of guidance, control, and dynamics. 2011, Vol 34, Num 3, pp 820-831, issn 0731-5090, 12 p.Article
In-orbit repositioning of multiple solar sail spacecraftMENGALI, Giovanni; QUARTA, Alessandro A.Aerospace science and technology. 2008, Vol 12, Num 7, pp 506-514, issn 1270-9638, 9 p.Article
Precise relativistic orbits in Kerr and Kerr-(anti) de Sitter spacetimesKRANIOTIS, G. V.Classical and quantum gravity (Print). 2004, Vol 21, Num 19, pp 4743-4769, issn 0264-9381, 27 p.Article
The laser astrometric test of a relativity missionTURYSHEV, Slava G; SHAO, Michael; NORDTVEDT, Kenneth et al.Classical and quantum gravity (Print). 2004, Vol 21, Num 12, pp 2273-2799, issn 0264-9381, 527 p.Article
Inverse solar sail trajectory problemMCINNES, Colin R.Journal of guidance, control, and dynamics. 2003, Vol 26, Num 2, pp 369-371, issn 0731-5090, 3 p.Article
Dynamical evolution of Jupiter's Trojan asteroidsLEVISON, H. F; SHOEMAKER, E. M; SHOEMAKER, C. S et al.Nature (London). 1997, Vol 385, Num 6611, pp 42-44, issn 0028-0836Article
Sur quelques méthodes itératives et universelles de calcul d'orbites de mouvements Képleriens perturbés ou non = Some unified iterative methods in orbit determination of pure or perturbed Keplerian motionDumoulin, Christian; Rapaport, Michel.1994, 252 p.Thesis
Correlation of Optical Observations of Earth-Orbiting Objects and Initial Orbit DeterminationFUJIMOTO, K; SCHEERES, D. J.Journal of guidance, control, and dynamics. 2012, Vol 35, Num 1, pp 208-221, issn 0731-5090, 14 p.Article
Optimal Lunar Orbit Insertion from a Variable Symmetric Free-Return TrajectoryJESICK, Mark; OCAMPO, Cesar.Journal of guidance, control, and dynamics. 2011, Vol 34, Num 6, pp 1867-1875, issn 0731-5090, 9 p.Article
Particle Swarm Optimization Applied to Space TrajectoriesPONTANI, Mauro; CONWAY, Bruce A.Journal of guidance, control, and dynamics. 2010, Vol 33, Num 5, pp 1429-1441, issn 0731-5090, 13 p.Article
Periodic orbits with low-thrust propulsion in the restricted three-body problemMORIMOTO, Mutsuko; YAMAKAWA, Hiroshi; UESUGI, Kuninori et al.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 5, pp 1131-1139, issn 0731-5090, 9 p.Article
Planet-planet scattering in the upsilon Andromedae systemFORD, Eric B; LYSTAD, Verene; RASIO, Frederic A et al.Nature (London). 2005, Vol 434, Num 7035, pp 873-876, issn 0028-0836, 4 p.Article
Orbits of 10 interferometric binary systems calculated by using the improved Koval'skij methodOLEVIC, D; CVETKOVIC, Z.Astronomy and astrophysics (Berlin. Print). 2004, Vol 415, Num 1, pp 259-264, issn 0004-6361, 6 p.Article
Orbital dynamics about a slowly rotating asteroidHOWARD, J. E; WILKERSON, T. D; CANTRELL, J. N et al.Geophysical research letters. 2002, Vol 29, Num 8, pp 94.1-94.3, issn 0094-8276Article
Asteroid hazard mitigation using the yarkovsky effect : The rice genomeSPITALE, Joseph N.Science (Washington, D.C.). 2002, Vol 296, Num 5565, issn 0036-8075, p. 77Article
Fracture of solids by radiation pulses as a method of ensuring safety in spaceGALIEV, SH. U; ZHURAKHOVSKII, S. V; IVASHCHENKO, K. B et al.Strength of materials. 1996, Vol 28, Num 3, pp 186-201, issn 0039-2316Article
Three-body effects in the PSR 1257 + 12 planetary systemRENU MALHOTRA.The Astrophysical journal. 1993, Vol 407, Num 1, pp 266-275, issn 0004-637X, 1Article
Design and verification of a magnetometer-based orbit determination and sensor calibration algorithmJUANG, Jyh-Ching; TSAI, Yung-Fu; TSAI, Chiu-Teng et al.Aerospace science and technology (Imprimé). 2012, Vol 21, Num 1, pp 47-54, issn 1270-9638, 8 p.Article
Ion Beam Shepherd for Contactless Space Debris RemovalBOMBARDELLI, Claudio; PELAEZ, Jesus.Journal of guidance, control, and dynamics. 2011, Vol 34, Num 3, pp 916-920, issn 0731-5090, 5 p.Article
Approximate Analytical Solutions to Optimal Reconfiguration Problems in Perturbed Satellite Relative MotionLEE, Sangjin; PARK, Sang-Young.Journal of guidance, control, and dynamics. 2011, Vol 34, Num 4, pp 1097-1111, issn 0731-5090, 15 p.Article
Evidence for a past high-eccentricity lunar orbitGARRICK-BETHELL, Ian; WISDOM, Jack; ZUBER, Maria T et al.Science (Washington, D.C.). 2006, Vol 313, Num 5787, pp 652-655, issn 0036-8075, 4 p.Article
Forced resonant migration of Pluto's outer satellites by charonWARD, William R; CANUP, Robin M.Science (Washington, D.C.). 2006, Vol 313, Num 5790, pp 1107-1109, issn 0036-8075, 3 p.Article
Les caprices du satellite = The whims of a satelliteAUDIN, Michèle.Pour la science. 2004, Num 317, pp 70-74, issn 0153-4092, 5 p.Article
Mechanism for precision orbit control with applications to formation keepingROSS, I. Michael.Journal of guidance, control, and dynamics. 2002, Vol 25, Num 4, pp 818-820, issn 0731-5090Article