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Results:
1-9
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Results: 9
Authors:
WILSON RS
HOWELL KC
Citation: Rs. Wilson et Kc. Howell, TRAJECTORY DESIGN IN THE SUN-EARTH-MOON SYSTEM USING LUNAR GRAVITY ASSISTS, Journal of spacecraft and rockets, 35(2), 1998, pp. 191-198
Authors:
ELY TA
HOWELL KC
Citation: Ta. Ely et Kc. Howell, DYNAMICS OF ARTIFICIAL-SATELLITE ORBITS WITH TESSERAL RESONANCES INCLUDING THE EFFECTS OF LUNI-SOLAR PERTURBATIONS, Dynamics and stability of systems, 12(4), 1997, pp. 243-269
Authors:
HOWELL KC
BARDEN BT
LO MW
Citation: Kc. Howell et al., APPLICATION OF DYNAMICAL-SYSTEMS THEORY TO TRAJECTORY DESIGN FOR A LIBRATION POINT MISSION, The Journal of the astronautical sciences, 45(2), 1997, pp. 161-178
Authors:
HIDAYJOHNSTON LA
HOWELL KC
Citation: La. Hidayjohnston et Kc. Howell, IMPULSIVE TIME-FREE TRANSFERS BETWEEN HALO ORBITS, Celestial mechanics & dynamical astronomy, 64(4), 1996, pp. 281-303
Authors:
ELY TA
HOWELL KC
Citation: Ta. Ely et Kc. Howell, LONG-TERM EVOLUTION OF ARTIFICIAL-SATELLITE ORBITS DUE TO RESONANT TESSERAL HARMONICS, The Journal of the astronautical sciences, 44(2), 1996, pp. 167-190
Authors:
HIDAYJOHNSTON LA
HOWELL KC
Citation: La. Hidayjohnston et Kc. Howell, TRANSFERS BETWEEN CALIBRATION-POINT ORBITS IN THE ELLIPTIC RESTRICTEDPROBLEM, Celestial mechanics & dynamical astronomy, 58(4), 1994, pp. 317-337
Authors:
HOWELL KC
HIDAYJOHNSTON LA
Citation: Kc. Howell et La. Hidayjohnston, TIME-FREE TRANSFERS BETWEEN LIBRATION-POINT ORBITS IN THE ELLIPTIC RESTRICTED PROBLEM, Acta astronautica, 32(4), 1994, pp. 245-254
Authors:
HOWELL KC
GORDON SC
Citation: Kc. Howell et Sc. Gordon, ORBIT DETERMINATION ERROR ANALYSIS AND A STATION-KEEPING STRATEGY FORSUN-EARTH L(1) LIBRATION POINT ORBITS, The Journal of the astronautical sciences, 42(2), 1994, pp. 207-228
Authors:
HOWELL KC
FARQUHAR RW
Citation: Kc. Howell et Rw. Farquhar, BREAKWELL,JOHN, THE RESTRICTED PROBLEM, AND HALO ORBITS, Acta astronautica, 29(6), 1993, pp. 485-488
Risultati:
1-9
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