메뉴 건너뛰기




Volumn 1, Issue , 2004, Pages 533-540

Mission design for the MMS tetrahedron formation

Author keywords

[No Author keywords available]

Indexed keywords

BUDGET CONTROL; ERROR ANALYSIS; FLIGHT DYNAMICS; FUEL CONSUMPTION; MAGNETIC FIELDS; OPTIMIZATION; SPACECRAFT; TRAJECTORIES;

EID: 11244337965     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (17)

References (12)
  • 2
    • 0008836685 scopus 로고
    • A general timing condition for consecutive collision orbits in the limiting case μ, = 0 of the elliptic restricted three-body problem
    • K. Howell and S. Marsh, "A General Timing Condition for Consecutive Collision Orbits in the Limiting Case μ, = 0 of the Elliptic Restricted Three-Body Problem," Celestial Mechanics, Vol. 52, No. 2, 1991, pp. 167-194.
    • (1991) Celestial Mechanics , vol.52 , Issue.2 , pp. 167-194
    • Howell, K.1    Marsh, S.2
  • 4
    • 11244279132 scopus 로고    scopus 로고
    • Trajectory design of Phases 3 and 4 of MMS
    • August 16. NASA Goddard Space Flight Center, Greenbelt, Maryland
    • A. Edery and J. Guzmán, "Trajectory Design of Phases 3 and 4 of MMS," Presentation to the MMS Project, August 16 2002. NASA Goddard Space Flight Center, Greenbelt, Maryland.
    • (2002) MMS Project
    • Edery, A.1    Guzmán, J.2
  • 5
    • 1542357420 scopus 로고    scopus 로고
    • Designing phase 2 for the double-lunar swingby of the magnetospheric multiscale mission (MMS)
    • Ponce, Puerto Rico, February 9-13. AAS 03-245
    • A. Edery, "Designing Phase 2 for the Double-Lunar Swingby of the Magnetospheric Multiscale Mission (MMS)," 13th Space Flight Mechanics Meeting, Ponce, Puerto Rico, February 9-13 2003. AAS 03-245.
    • (2003) 13th Space Flight Mechanics Meeting
    • Edery, A.1
  • 8
    • 11444269137 scopus 로고    scopus 로고
    • Flying a four-spacecraft formation by the moon...twice
    • Ponce, Puerto Rico, February 9-132003. AAS 03-132
    • J. Guzmán and A. Edery, "Flying a Four-Spacecraft Formation by the Moon...Twice," 13th Space Flight Mechanics Meeting, Ponce, Puerto Rico, February 9-132003. AAS 03-132.
    • 13th Space Flight Mechanics Meeting
    • Guzmán, J.1    Edery, A.2
  • 9
    • 11244356039 scopus 로고    scopus 로고
    • Tetrahedron formation control
    • Greenbelt, Maryland, NASA Goddard Space Flight Center, October 28-30
    • J. Guzmán, 'Tetrahedron Formation Control," GSFC Flight Mechanics Symposium, Greenbelt, Maryland, NASA Goddard Space Flight Center, October 28-30 2003.
    • (2003) GSFC Flight Mechanics Symposium
    • Guzmán, J.1
  • 10
    • 11244264929 scopus 로고    scopus 로고
    • The magnetospheric multi-scale mission: An electronically tethered constellation of four spacecraft
    • Pisa, Italy, International Astronautical Federation, February 24-26
    • S. Curds, C. Petruzzo, P. Clark, and A. Peterson, "The Magnetospheric Multi-Scale Mission: An Electronically Tethered Constellation of Four Spacecraft," 3rd International Workshop on Satellite Constellations and Formation Flying, Pisa, Italy, International Astronautical Federation, February 24-26 2003.
    • (2003) 3rd International Workshop on Satellite Constellations and Formation Flying
    • Curds, S.1    Petruzzo, C.2    Clark, P.3    Peterson, A.4
  • 11
    • 19644367850 scopus 로고    scopus 로고
    • Formation tetrahedron design for phase 1 of the magnetospheric multi-scale mission
    • Green-belt, Maryland, NASA Goddard Space Flight Center, October 28-30
    • S. Hughes, "Formation Tetrahedron Design for Phase 1 of the Magnetospheric Multi-Scale Mission," GSFC Flight Mechanics Symposium, Green-belt, Maryland, NASA Goddard Space Flight Center, October 28-30 2003.
    • (2003) GSFC Flight Mechanics Symposium
    • Hughes, S.1
  • 12
    • 0141649231 scopus 로고    scopus 로고
    • A comparison of trajectory optimization methods for the impulsive minimum fuel rendezvous problem
    • Breckenridge, Colorado, February 5-9. AAS 03-006
    • S. Hughes, L. Mailhe, and J. Guzmán, "A Comparison of Trajectory Optimization Methods for the Impulsive Minimum Fuel Rendezvous Problem," 26th Annual AAS Guidance and Control Conference, Breckenridge, Colorado, February 5-9 2003. AAS 03-006.
    • (2003) 26th Annual AAS Guidance and Control Conference
    • Hughes, S.1    Mailhe, L.2    Guzmán, J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.