| Year |
Citation |
Score |
| 2019 |
Mahajan B, Vadali SR, Alfriend KT. State-Transition Matrix for Satellite Relative Motion in the Presence of Gravitational Perturbations Journal of Guidance Control and Dynamics. 42: 1441-1457. DOI: 10.2514/1.G004133 |
0.46 |
|
| 2019 |
Mahajan B, Alfriend KT. Analytic orbit theory with any arbitrary spherical harmonic as the dominant perturbation Celestial Mechanics and Dynamical Astronomy. 131: 45. DOI: 10.1007/S10569-019-9923-3 |
0.371 |
|
| 2018 |
Mahajan B, Vadali SR, Alfriend KT. Exact Delaunay normalization of the perturbed Keplerian Hamiltonian with tesseral harmonics Celestial Mechanics and Dynamical Astronomy. 130: 25. DOI: 10.1007/S10569-018-9818-8 |
0.468 |
|
| 2016 |
Zeng X, Gong S, Li J, Alfriend KT. Solar sail body-fixed hovering over elongated asteroids Journal of Guidance, Control, and Dynamics. 39: 1223-1231. DOI: 10.2514/1.G001061 |
0.379 |
|
| 2015 |
Schumacher PW, Sabol C, Higginson CC, Alfriend KT. Uncertain lambert problem Journal of Guidance, Control, and Dynamics. 38: 1573-1584. DOI: 10.2514/1.G001019 |
0.404 |
|
| 2015 |
Fujimoto K, Alfriend KT. Optical short-arc association hypothesis gating via angle-rate information Journal of Guidance, Control, and Dynamics. 38: 1602-1613. DOI: 10.2514/1.G000927 |
0.325 |
|
| 2014 |
Zeng X, Alfriend KT, Vadali SR. Solar sail planar multireversal periodic orbits Journal of Guidance, Control, and Dynamics. 37: 674-681. DOI: 10.2514/1.58598 |
0.426 |
|
| 2014 |
Holzinger MJ, Alfriend KT, Wetterer CJ, Luu KK, Sabol C, Hamada K. Photometric attitude estimation for agile space objects with shape uncertainty Journal of Guidance, Control, and Dynamics. 37: 921-932. DOI: 10.2514/1.58002 |
0.348 |
|
| 2014 |
Weisman RM, Majji M, Alfriend KT. Analytic characterization of measurement uncertainty and initial orbit determination on orbital element representations Celestial Mechanics and Dynamical Astronomy. 1-31. DOI: 10.1007/S10569-013-9529-0 |
0.691 |
|
| 2014 |
Weisman RM, Majji M, Alfriend KT. Application of the transformation of variables technique for uncertainty mapping in nonlinear filtering Celestial Mechanics and Dynamical Astronomy. 1-36. DOI: 10.1007/S10569-013-9527-2 |
0.626 |
|
| 2014 |
Yan H, Vadali SR, Alfriend KT. State transition matrix for relative motion including higher-order gravity perturbations Advances in the Astronautical Sciences. 150: 1317-1336. |
0.373 |
|
| 2014 |
Yan H, Vadali SR, Alfriend KT. A simplified formulation of the satellite perturbed relative motion problem Aiaa/Aas Astrodynamics Specialist Conference 2014. |
0.412 |
|
| 2014 |
Yan H, Vadali SR, Alfriend KT. State Transition Matrix for relative motion including J2 and third-body perturbations Advances in the Astronautical Sciences. 152: 2479-2496. |
0.379 |
|
| 2013 |
Khutorovsky ZN, Samotokhin AS, Alfriend KT. Guaranteed approach for orbit determination with limited error measurements Journal of Guidance, Control, and Dynamics. 36: 1186-1193. DOI: 10.2514/1.56220 |
0.343 |
|
| 2013 |
Sabol C, Hill K, Alfriend K, Sukut T. Nonlinear effects in the correlation of tracks and covariance propagation Acta Astronautica. 84: 69-80. DOI: 10.1016/J.Actaastro.2012.08.023 |
0.392 |
|
| 2013 |
Roscoe CWT, Vadali SR, Alfriend KT, Desai UP. Satellite formation design in orbits of high eccentricity with performance constraints specified over a region of interest: MMS phase II Acta Astronautica. 82: 16-24. DOI: 10.1016/J.Actaastro.2012.07.028 |
0.414 |
|
| 2013 |
Roscoe CWT, Vadali SR, Alfriend KT. Third-body perturbation effects on satellite formations Advances in the Astronautical Sciences. 147: 483-502. DOI: 10.1007/S40295-015-0057-X |
0.465 |
|
| 2013 |
Zeng X, Alfriend KT, Vadali SR. Three-dimensional time Optimal Multi-reversal Orbit by Using Solar Sailing Journal of the Astronautical Sciences. 60: 378-395. DOI: 10.1007/S40295-015-0056-Y |
0.425 |
|
| 2013 |
Weisman RM, Majji M, Alfriend KT. Analytic characterization of measurement uncertainty and initial orbit determination on orbital element uncertainty and correlation Advances in the Astronautical Sciences. 148: 37-56. |
0.637 |
|
| 2012 |
Holzinger MJ, Scheeres DJ, Alfriend KT. Object correlation, maneuver detection, and characterization using control-distance metrics Journal of Guidance, Control, and Dynamics. 35: 1312-1325. DOI: 10.2514/1.53245 |
0.317 |
|
| 2012 |
Zeng X, Alfriend KT, Li J, Vadali SR. Optimal solar sail trajectory analysis for interstellar missions Advances in the Astronautical Sciences. 143: 1951-1964. DOI: 10.1007/S40295-014-0008-Y |
0.364 |
|
| 2012 |
Hill K, Sabol C, Alfriend KT. Comparison of Covariance Based Track Association Approaches Using Simulated Radar Data Journal of the Astronautical Sciences. 59: 281-300. DOI: 10.1007/S40295-013-0018-1 |
0.371 |
|
| 2012 |
Roscoe CWT, Vadali SR, Alfriend KT. Design of satellite formations in orbits of high eccentricity with performance constraints specified over a region of interest Journal of the Astronautical Sciences. 59: 145-164. DOI: 10.1007/S40295-013-0010-9 |
0.434 |
|
| 2012 |
Majji M, Weisman R, Alfriend KT. Solution of the Liouville's equation for Keplerian motion: Application to uncertainty calculations Advances in the Astronautical Sciences. 143: 2399-2408. |
0.644 |
|
| 2011 |
Fujimoto K, Scheeres DJ, Alfriend KT. Analytical non-linear propagation of uncertainty in the two-body problem Advances in the Astronautical Sciences. 140: 1439-1457. DOI: 10.2514/1.54385 |
0.378 |
|
| 2011 |
Sekhavat P, Yan H, Fleming A, Ross IM, Alfriend KT. Closed-loop time-optimal attitude maneuvering of magnetically actuated spacecraft Journal of the Astronautical Sciences. 58: 81-97. DOI: 10.1007/Bf03321160 |
0.319 |
|
| 2011 |
Weisman RM, Majji M, Alfriend KT. Analytic assessment of sensor uncertainty for application to space object tracking and correlation 62nd International Astronautical Congress 2011, Iac 2011. 3: 2323-2337. |
0.575 |
|
| 2010 |
Roscoe CWT, Vadali SR, Alfriend KT, Desai UP. Optimal formation design for the magnetospheric multiscale mission using differential orbital elements Aiaa/Aas Astrodynamics Specialist Conference 2010. DOI: 10.2514/1.52484 |
0.406 |
|
| 2010 |
Sengupta P, Vadali SR, Alfriend KT. Satellite orbit design and maintenance for terrestrial coverage Journal of Spacecraft and Rockets. 47: 177-187. DOI: 10.2514/1.44120 |
0.612 |
|
| 2009 |
Maruskin JM, Scheeres DJ, Alfriend KT. Correlation of optical observations of objects in Earth orbit Journal of Guidance, Control, and Dynamics. 32: 194-209. DOI: 10.2514/1.36398 |
0.362 |
|
| 2009 |
Yan H, Alfriend KT, Vadali SR, Sengupta P. Optimal design of satellite formation relative motion orbits using least-squares methods Journal of Guidance, Control, and Dynamics. 32: 599-604. DOI: 10.2514/1.35044 |
0.664 |
|
| 2008 |
Vadali SR, Sengupta P, Yan H, Alfriend KT. Fundamental frequencies of satellite relative motion and control of formations Journal of Guidance, Control, and Dynamics. 31: 1239-1248. DOI: 10.2514/1.34790 |
0.616 |
|
| 2008 |
Sengupta P, Vadali SR, Alfriend KT. Averaged relative motion and applications to formation flight near perturbed orbits Journal of Guidance, Control, and Dynamics. 31: 258-272. DOI: 10.2514/1.30620 |
0.646 |
|
| 2008 |
Yurasov VS, Nazarenko AI, Alfriend KT, Cefola PJ. Reentry time prediction using atmospheric density corrections Journal of Guidance, Control, and Dynamics. 31: 282-289. DOI: 10.2514/1.26593 |
0.335 |
|
| 2008 |
Vadali SR, Sengupta P, Yan H, Alfriend KT. On the fundamental frequencies of satellite relative motion and control of formations Advances in the Astronautical Sciences. 129: 2747-2766. |
0.36 |
|
| 2008 |
Vadali SR, Yan H, Alfriend KT. Formation maintenance and fuel balancing for satellites with impulsive control Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.397 |
|
| 2007 |
Yan H, Alfriend KT. Approximate minimum energy control laws for low-thrust formation reconfiguration Journal of Guidance, Control, and Dynamics. 30: 1182-1185. DOI: 10.2514/1.28494 |
0.406 |
|
| 2007 |
Yan H, Ross IM, Alfriend KT. Pseudospectral feedback control for three-axis magnetic attitude stabilization in elliptic orbits Journal of Guidance, Control, and Dynamics. 30: 1107-1115. DOI: 10.2514/1.26591 |
0.368 |
|
| 2007 |
Sabol C, Alfriend KT, Wiese D. Angles-only orbit updates for low-earth-orbit satellites Journal of Guidance, Control, and Dynamics. 30: 314-321. DOI: 10.2514/1.25008 |
0.427 |
|
| 2007 |
How JP, Breger LS, Mitchell M, Alfriend KT, Carpenter R. Differential semimajor axis estimation performance using carrier-phase differential global positioning system measurements Journal of Guidance, Control, and Dynamics. 30: 301-313. DOI: 10.2514/1.23083 |
0.338 |
|
| 2007 |
Lee DJ, Alfriend KT. Sigma point filtering for sequential orbit estimation and prediction Journal of Spacecraft and Rockets. 44: 388-398. DOI: 10.2514/1.20702 |
0.541 |
|
| 2007 |
Sengupta P, Vadali SR, Alfriend KT. Second-order state transition for relative motion near perturbed, elliptic orbits Celestial Mechanics and Dynamical Astronomy. 97: 101-129. DOI: 10.1007/S10569-006-9054-5 |
0.646 |
|
| 2007 |
Wilkins MP, Sabol C, Cefola PJ, Alfriend KT. Validation and application of corrections to the NRLMSISE-00 atmospheric density model Advances in the Astronautical Sciences. 127: 1285-1304. |
0.715 |
|
| 2007 |
Wilkins MP, Sabol C, Cefola PJ, Alfriend KT. Improving dynamic calibration of the atmosphere Advances in the Astronautical Sciences. 127: 1257-1272. |
0.679 |
|
| 2007 |
Yan H, Alfriend KT, Vadali SR, Prasenjit S. Optimal design of satellite formation relative motion orbits using least squares methods Advances in the Astronautical Sciences. 127: 1467-1484. |
0.422 |
|
| 2006 |
Yan H, Alfriend KT. Numerical searches and optimal control of J2 invariant orbits Advances in the Astronautical Sciences. 124: 991-1009. |
0.302 |
|
| 2006 |
Wilkins MP, Sabol CA, Cefola PJ, Alfriend KT. Practical challenges in implementing atmospheric density corrections to the NRLMSISE-00 model Advances in the Astronautical Sciences. 124: 1113-1130. |
0.69 |
|
| 2005 |
Alfriend KT, Yan H. Evaluation and comparison of relative motion theories Journal of Guidance, Control, and Dynamics. 28: 254-261. DOI: 10.2514/1.6691 |
0.484 |
|
| 2005 |
Vaddi SS, Alfriend KT, Vadali SR, Sengupta P. Formation establishment and reconfiguration using impulsive control Journal of Guidance, Control, and Dynamics. 28: 262-268. DOI: 10.2514/1.6687 |
0.6 |
|
| 2005 |
Gim DW, Alfriend KT. Satellite relative motion using differential equinoctial elements Celestial Mechanics and Dynamical Astronomy. 92: 295-336. DOI: 10.1007/S10569-004-1799-0 |
0.809 |
|
| 2005 |
Gim DW, Alfriend KT. Criteria for best configuration and sub-optimal reconfiguration for MMS mission Advances in the Astronautical Sciences. 119: 947-968. |
0.796 |
|
| 2005 |
Yan H, Sengupta P, Vadali SR, Alfriend KT. Development of a state transition matrix for relative motion using the unit sphere approach Advances in the Astronautical Sciences. 119: 935-946. |
0.433 |
|
| 2004 |
Sengupta P, Vadali SR, Alfriend KT. Modeling and control of satellite formations in high eccentricity orbits Journal of the Astronautical Sciences. 52: 149-168. DOI: 10.1007/Bf03546426 |
0.658 |
|
| 2003 |
Gim DW, Alfriend KT. State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit Journal of Guidance, Control, and Dynamics. 26: 956-971. DOI: 10.2514/2.6924 |
0.809 |
|
| 2003 |
Lee DJ, No TS, Choi SW, Lee SR, Kim HJ, Alfriend KT. Precise Ephemeris Reconstruction Using the Clohessy-Wiltshire Frame and Multiple Sequential Compressions Journal of Guidance, Control, and Dynamics. 26: 781-785. DOI: 10.2514/2.5112 |
0.61 |
|
| 2003 |
Carpenter JR, Alfriend KT. Navigation accuracy guidelines for orbital formation flying Aiaa Guidance, Navigation, and Control Conference and Exhibit. DOI: 10.1007/Bf03546351 |
0.466 |
|
| 2003 |
Vaddi SS, Vadali SR, Alfriend KT. Formation flying: Accommodating nonlinearity and eccentricity perturbations Journal of Guidance, Control, and Dynamics. 26: 214-223. |
0.366 |
|
| 2002 |
Vaddi SS, Vadali SR, Alfriend KT. Formation flying: Accommodating non-linearity and eccentricity perturbations Advances in the Astronautical Sciences. 112: 985-1004. DOI: 10.2514/2.5054 |
0.501 |
|
| 2002 |
Alfriend KT, Lee DJ, Glenn Creamer N. Optimal servicing of geosynchronous satellites Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. DOI: 10.2514/1.15602 |
0.591 |
|
| 2002 |
Vadali SR, Vaddi SS, Alfriend KT. An intelligent control concept for formation flying satellites International Journal of Robust and Nonlinear Control. 12: 97-115. DOI: 10.1002/Rnc.678 |
0.492 |
|
| 2002 |
Gim DW, Alfriend KT. The state transition matrix for relative motion of formation flying satellites Advances in the Astronautical Sciences. 112: 1021-1042. |
0.794 |
|
| 2002 |
Alfriend KT, Yan H, Vadali SR. Nonlinear considerations in satellite formation flying Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.341 |
|
| 2002 |
Wilkins MP, Subbarao K, Alfriend KT, Vadali SR. Modeling and simulation of a Sail Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. |
0.705 |
|
| 2002 |
Alfriend KT, Gim DW, Vadali SR. The characterization of formation flying satellite relative motion orbits Advances in the Astronautical Sciences. 112: 577-583. |
0.801 |
|
| 2002 |
Lee DJ, No TS, Baek JB, Lee SR, Kim HJ, Alfriend KT. Precise onboard ephemeris propagation method using CW frame and multiple compressions Advances in the Astronautical Sciences. 112: 441-455. |
0.335 |
|
| 2001 |
Schaub H, Alfriend KT. Impulsive feedback control to establish specific mean orbit elements of spacecraft formations Journal of Guidance, Control, and Dynamics. 24: 739-745. DOI: 10.2514/2.4774 |
0.479 |
|
| 2001 |
Alfriend KT, Vadali SR, Schaub H. Formation flying satellites: Control by an astrodynamicist Celestial Mechanics and Dynamical Astronomy. 81: 57-62. DOI: 10.1023/A:1013307103630 |
0.389 |
|
| 2001 |
Schaub H, Alfriend KT. J2 invariant relative orbits for spacecraft formations Celestial Mechanics and Dynamical Astronomy. 79: 77-95. DOI: 10.1023/A:1011161811472 |
0.413 |
|
| 2001 |
Gim DW, Alfriend KT. The state transition matrix of relative motion for the perturbed non-circular reference orbit Advances in the Astronautical Sciences. 108: 913-924. |
0.815 |
|
| 2001 |
Alfriend KT, Vadali SR, Wilkins MP. Dynamics and control of Power Sail Advances in the Astronautical Sciences. 108: 1791-1810. |
0.682 |
|
| 2000 |
Schaub H, Alfriend KT. Hybrid Cartesian and orbit element feedback law for formation flying spacecraft Astrodynamics Specialist Conference. 184-191. DOI: 10.2514/2.4893 |
0.475 |
|
| 2000 |
Akella MR, Alfriend KT. Probability of collision between space objects Journal of Guidance, Control, and Dynamics. 23: 769-772. DOI: 10.2514/2.4611 |
0.39 |
|
| 2000 |
Alfriend KT, Schaub H. Dynamic and control of spacecraft formations: Challenges and some solutions Journal of the Astronautical Sciences. 48: 249-267. DOI: 10.1007/Bf03546279 |
0.484 |
|
| 2000 |
Schaub H, Vadali SR, Junkins JL, Alfriend KT. Spacecraft formation flying control using mean orbit elements Advances in the Astronautical Sciences. 103: 163-181. DOI: 10.1007/Bf03546219 |
0.443 |
|
| 2000 |
Wilkins MP, Alfriend KT. Characterizing orbit uncertainty due to atmospheric uncertainty Astrodynamics Specialist Conference. 19-29. |
0.714 |
|
| 2000 |
Schaub H, Alfriend KT. Impulsive spacecraft formation flying control to establish specific mean orbit elements Advances in the Astronautical Sciences. 105: 207-220. |
0.357 |
|
| 2000 |
Alfriend KT, Schaub H. Dynamics and control of spacecraft formations: Challenges and some solutions Advances in the Astronautical Sciences. 106: 205-223. |
0.384 |
|
| 2000 |
Alfriend KT, Wilkins MP. Covariance as an estimator of orbit prediction error growth in the presence of unknown sensor biases Advances in the Astronautical Sciences. 103: 1913-1921. |
0.702 |
|
| 2000 |
Lee DJ, Alfriend KT. Effect of atmospheric density uncertainty on collision probability Advances in the Astronautical Sciences. 105: 1255-1272. |
0.31 |
|
| 2000 |
Vadali SR, Alfriend KT, Vaddi S. Hill's equations, mean orbital elements, andformation flying of satellites Advances in the Astronautical Sciences. 106: 187-203. |
0.378 |
|
| 2000 |
Alfriend KT, Schaub H, Gim DW. Gravitational perturbations, nonlinearity and circular orbit assumption effects on formation flying control strategies Advances in the Astronautical Sciences. 104: 139-155. |
0.795 |
|
| 1999 |
Alfriend KT, Akella MR, Frisbee J, Foster JL, Lee D, Wilkins M. Probability of Collision Error Analysis Space Debris. 1: 21-35. DOI: 10.1023/A:1010056509803 |
0.745 |
|
| 1999 |
Vadali SR, Schaub H, Alfriend KT. Initial conditions and fuel-optimal control for formation flying of satellites 1999 Guidance, Navigation, and Control Conference and Exhibit. 1-11. |
0.305 |
|
| 1998 |
Beaulieu MR, Alfriend KT, Jerardi T. Launch detection satellite system engineering error analysis Journal of Spacecraft and Rockets. 35: 487-495. DOI: 10.2514/2.3357 |
0.337 |
|
| 1997 |
Akella MR, Junkins JL, Alfriend KT. Some consequences of force model uncertainty on probability of collision with orbital debris Advances in the Astronautical Sciences. 97: 111-121. |
0.356 |
|
| 1996 |
Chang CO, Liu LZ, Alfriend KT. Dynamics and stability of a freely precessing spacecraft containing a nutation damper Journal of Guidance, Control, and Dynamics. 19: 297-304. DOI: 10.2514/3.21618 |
0.417 |
|
| 1995 |
Ross IM, Alfriend KT. Low-Earth-orbit maintenance - Reboost vs thrust-drag cancellation Journal of Guidance Control and Dynamics. 18: 930-932. DOI: 10.2514/3.21486 |
0.375 |
|
| 1994 |
Alfriend KT, Lewis DL. Estimation of the low-Earth-orbit debris population and distribution Journal of Spacecraft and Rockets. 31: 48-53. DOI: 10.2514/3.26401 |
0.328 |
|
| 1984 |
Alfriend KT, Coffey SL. Elimination of the perigee in the satellite problem Celestial Mechanics. 32: 163-172. DOI: 10.1007/Bf01231123 |
0.304 |
|
| 1981 |
Longman RW, Alfriend KT. Actuator placement from degree of controllability criteria for regular slewing of flexible spacecraft Acta Astronautica. 8: 703-718. DOI: 10.1016/0094-5765(81)90012-6 |
0.339 |
|
| 1979 |
Longman RW, Alfriend KT. Optimal Control of Large Angle Attitude Maneuvers for Flexible Spacecraft Ifac Proceedings Volumes. 12: 57-62. DOI: 10.1016/S1474-6670(17)65716-1 |
0.333 |
|
| 1978 |
Kaufman B, Alfriend KT, Dasenbrock RR. Luni-solar perturbations in the extended phase space representation of the Vinti problem Acta Astronautica. 5: 727-744. DOI: 10.1016/0094-5765(78)90065-6 |
0.368 |
|
| 1977 |
Alfriend KT. Comment on 'Analytical solution for planar librations of a gravity stabilized satellite' Journal of Spacecraft and Rockets. 14: 767-768. DOI: 10.2514/3.27995 |
0.344 |
|
| 1977 |
Alfriend KT, Dasenbrock R, Pickard H, Deprit A. The extended phase space formulation of the Vinti problem Celestial Mechanics. 16: 441-458. DOI: 10.1007/Bf01229287 |
0.382 |
|
| 1976 |
Stickler AC, Alfriend KT. ELEMENTARY MAGNETIC ATTITUDE CONTROL SYSTEM Journal of Spacecraft and Rockets. 13: 282-287. DOI: 10.2514/3.57089 |
0.366 |
|
| 1975 |
Alfriend KT. Magnetic attitude control system for dual-spin satellites Aiaa Journal. 13: 817-822. DOI: 10.2514/3.60443 |
0.395 |
|
| 1975 |
Alfriend KT. Method for evaluating gravity effects in the testing of nutation dampers Journal of Spacecraft and Rockets. 12: 359-362. DOI: 10.2514/3.27841 |
0.308 |
|
| 1975 |
Alfriend KT, Velez CE. The application of general perturbation theories to the artificial satellite problem Acta Astronautica. 2: 577-591. DOI: 10.1016/0094-5765(75)90003-X |
0.431 |
|
| 1974 |
Alfriend KT, Hubert CH. Stability of a Dual-Spin Satellite with Two Dampers Journal of Spacecraft and Rockets. 11: 469-474. DOI: 10.2514/3.62108 |
0.401 |
|
| 1974 |
Alfriend KT. Partially Filled Viscous Ring Nutation Damper Journal of Spacecraft and Rockets. 11: 456-462. DOI: 10.2514/3.62106 |
0.368 |
|
| 1972 |
Alfriend KT. A nonlinear stability problem in the three dimensional restricted three body problem Celestial Mechanics. 5: 502-511. DOI: 10.1007/Bf01464776 |
0.409 |
|
| 1971 |
Alfriend KT. Stability and motion in two degree of freedom hamiltonian systems for three-to-one commensurability International Journal of Non-Linear Mechanics. 6: 563-568. DOI: 10.1016/0020-7462(71)90020-5 |
0.409 |
|
| 1971 |
Alfriend KT. Stability of and motion about L4 at three-to-one commensurability Celestial Mechanics. 4: 60-77. DOI: 10.1007/Bf01230322 |
0.375 |
|
| 1971 |
Alfriend KT. Stability and motion in two degree-of-freedom hamiltonian systems for two-to-one commensurability Celestial Mechanics. 3: 247-265. DOI: 10.1007/Bf01228038 |
0.42 |
|
| 1970 |
Alfriend KT. The stability of the triangular Lagrangian points for commensurability of order two Celestial Mechanics. 1: 351-359. DOI: 10.1007/Bf01231140 |
0.346 |
|
| 1969 |
Alfriend KT, Rand RH. Stability of the triangular points in the elliptic restricted problem of three bodies. Aiaa Journal. 7: 1024-1028. DOI: 10.2514/3.5270 |
0.357 |
|
| 1969 |
Alfriend KT, Kashiwagi Y. Minimum-time orbital rendezvous between neighboring elliptic orbits Journal of Optimization Theory and Applications. 4: 260-276. DOI: 10.1007/Bf00927950 |
0.361 |
|
| 1967 |
Davis RT, Alfriend KT. Solutions to Van der Pol's equation using a perturbation method International Journal of Non-Linear Mechanics. 2: 153-162. DOI: 10.1016/0020-7462(67)90011-X |
0.366 |
|
| Show low-probability matches. |