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Volumn 44, Issue 4, 1996, Pages 467-489

Refinement of a sun-synchronous, critically inclined orbit for the ELLIPSO™ personal communication system

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; FUEL ECONOMY; ORBITS; RADIATION EFFECTS; RESONANCE;

EID: 0030257129     PISSN: 00219142     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (19)

References (23)
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    • 0041011573 scopus 로고
    • Application of Sun-Synchronous, Critically Inclined Orbits to Global Personal Communications Systems
    • Paper No. 95-222, Albuquerque, New Mexico, February
    • SABOL, C. A., CEFOLA, P. J., and METZINGER, R. W. "Application of Sun-Synchronous, Critically Inclined Orbits to Global Personal Communications Systems," Paper No. 95-222, AAS/AIAA Spaceflight Mechanics Conference, Albuquerque, New Mexico, February 1995.
    • (1995) AAS/AIAA Spaceflight Mechanics Conference
    • Sabol, C.A.1    Cefola, P.J.2    Metzinger, R.W.3
  • 7
    • 0008860988 scopus 로고
    • Contract NAS 5-31500, Task 213, July
    • COMPUTER SCIENCES CORP. and NASA GODDARD SPACE FLIGHT CENTER (editors), GTDS Mathematical Theory Revision 1, Contract NAS 5-31500, Task 213, July 1989.
    • (1989) GTDS Mathematical Theory Revision 1
  • 8
    • 3342973731 scopus 로고
    • M.S. Thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts, June
    • FONTE, D. J. "Implementing a 50 × 50 Gravity Field Model in an Orbit Determination System," M.S. Thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts, June 1993.
    • (1993) Implementing a 50 × 50 Gravity Field Model in an Orbit Determination System
    • Fonte, D.J.1
  • 9
    • 0005743239 scopus 로고
    • The RADARSAT Flight Dynamics System: An Extensible, Portable, Workstation-based Mission Support System
    • Paper No. 94-3726, Scottsdale, Arizona, August
    • CEFOLA, P., PROULX, R., METZINGER, R., COHEN, M., and CARTER, D. "The RADARSAT Flight Dynamics System: An Extensible, Portable, Workstation-based Mission Support System," Paper No. 94-3726, AIAA/AAS Astrodynamics Specialist Conference, Scottsdale, Arizona, August 1994.
    • (1994) AIAA/AAS Astrodynamics Specialist Conference
    • Cefola, P.1    Proulx, R.2    Metzinger, R.3    Cohen, M.4    Carter, D.5
  • 10
    • 0039233611 scopus 로고
    • PC Based Orbit Determination
    • Paper No. 94-3776, Scottsdale, Arizona, August
    • FONTE, D. J. "PC Based Orbit Determination," Paper No. 94-3776, AIAA/AAS Astrodynamics Specialist Conference, Scottsdale, Arizona, August 1994.
    • (1994) AIAA/AAS Astrodynamics Specialist Conference
    • Fonte, D.J.1
  • 13
    • 0039233606 scopus 로고
    • Optimal DSST Input Decks for Various Orbit Types
    • PL-TR-95-1072, June
    • FONTE, D. J., and SABOL, C. A. "Optimal DSST Input Decks for Various Orbit Types," Phillips Lab Technical Report, PL-TR-95-1072, June 1995.
    • (1995) Phillips Lab Technical Report
    • Fonte, D.J.1    Sabol, C.A.2
  • 16
    • 3342921722 scopus 로고
    • M.S. Thesis submitted to the Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts, June
    • WALLACE, S. T. "Parallel Orbit Propagation and the Analysis of Satellite Constellation," M.S. Thesis submitted to the Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts, June 1995.
    • (1995) Parallel Orbit Propagation and the Analysis of Satellite Constellation
    • Wallace, S.T.1
  • 17
    • 0027719238 scopus 로고
    • A Historical Survey of Earth Gravitational Models used in Astrodynamics from Sputnik and Transit to GPS and TOPEX
    • VETTER, J. R., NEREM, R. S., CEFOLA, P. J., and HAGAR, H. "A Historical Survey of Earth Gravitational Models used in Astrodynamics from Sputnik and Transit to GPS and TOPEX," Advances in the Astronautical Sciences, Vol. 85, 1993, pp. 1233-1251.
    • (1993) Advances in the Astronautical Sciences , vol.85 , pp. 1233-1251
    • Vetter, J.R.1    Nerem, R.S.2    Cefola, P.J.3    Hagar, H.4
  • 18
    • 0001005159 scopus 로고
    • An Analytic Model for Upper Atmosphere Densities Based upon Jacchia's 1970 Models
    • December
    • ROBERTS, E. R., JR. "An Analytic Model for Upper Atmosphere Densities Based upon Jacchia's 1970 Models," Celestial Mechanics, Vol. 4, December 1971, pp. 368-377.
    • (1971) Celestial Mechanics , vol.4 , pp. 368-377
    • Roberts Jr., E.R.1
  • 21
    • 0026243381 scopus 로고
    • Calculating Satellite Umbra/Penumbra Entry and Exit Position and Times
    • October-December
    • MULLINS, L. D. "Calculating Satellite Umbra/Penumbra Entry and Exit Position and Times," Journal of the Astronautical Sciences, Vol. 39, No. 4, October-December 1991, pp. 411-422.
    • (1991) Journal of the Astronautical Sciences , vol.39 , Issue.4 , pp. 411-422
    • Mullins, L.D.1
  • 23
    • 5544258704 scopus 로고    scopus 로고
    • Optimal Orbit Transfer to a SunSynchronous, Critically Inclined Orbit for the ELLIPSO™ Personal Communication System
    • Paper No. 96-3615, San Diego, California, July
    • DRAIM, J. E., SABOL, C. A., and CEFOLA, P. J. "Optimal Orbit Transfer to a SunSynchronous, Critically Inclined Orbit for the ELLIPSO™ Personal Communication System," Paper No. 96-3615, AAS/AIAA Astrodynamics Specialist Conference, San Diego, California, July 1996.
    • (1996) AAS/AIAA Astrodynamics Specialist Conference
    • Draim, J.E.1    Sabol, C.A.2    Cefola, P.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.