Overcoming Genesis mission design challenges

Acta Astronautica

Volumn 52, Issue 2-6, 2003, Pages 281-287

  Williams, Kenneth E ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EARTH (PLANET); ORBITS; SPACECRAFT; SPACECRAFT PROPULSION; SUN; WIND;

SOLAR WIND SAMPLES;

SPACE RESEARCH;

EID: 0037237813     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(02)00167-4     Document Type: Conference Paper

References (5)

1. M.W. Lo, et al., Genesis Mission design, AIAA 98-4468, AIAA/AAS Astrodynamics Conference, Boston, MA, August 10-12, 1998.
2. J.L. Bell, M.W. Lo, R.S. Wilson, Genesis Trajectory design, AAS 99-398, AAS/AIAA Astrodynamics Specialist Conference, Girdwood, AK, August 16-19, 1999.
3. K.E. Williams, P.E. Hong, D. Han, Maneuver design and calibration for the Genesis spacecraft, AAS 99-399, AAS/AIAA Astrodynamics Specialist Conference, Girdwood, AK, August 16-19, 1999.
4. M.H. Bantell Jr., Control mode synthesis for Galileo spacecraft maneuvers, AIAA, 1980.
5. K.E. Williams, et al., Genesis Halo orbit station keeping design, to be presented at 15th International Symposium of Spaceflight Dynamics, Biarritz, France, June 26-30, 2000.