Autonomous navigation of high-earth satellites using celestial objects and doppler measurements

Astrodynamics Specialist Conference

Volumn , Issue , 2000, Pages 1-10

  Long, Anne C ^a   Leung, Dominic ^a   Folta, David ^b   Gramling, Cheryl ^b  

^a Computer Sciences Corporation ^*  (United States)

^b NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASTROPHYSICS; DOPPLER EFFECT; FLIGHT CONTROL SYSTEMS; NASA; NAVIGATION SYSTEMS; SATELLITE RELAY SYSTEMS; SPACE FLIGHT;

AUTONOMOUS NAVIGATION; AUTONOMOUS NAVIGATION SYSTEMS; COMMUNICATION COMPONENTS; DOPPLER MEASUREMENT; GODDARD SPACE FLIGHT CENTER; GUIDANCE , NAVIGATION , AND CONTROLS; NAVIGATION PERFORMANCE; TRACKING AND DATA RELAY SATELLITE SYSTEM;

ORBITS;

EID: 34249783811     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3937     Document Type: Conference Paper

References (7)

1. C. J. Gramling et al., "Preliminary Operational Results of the TDRSS Onboard Navigation System (TONS) for the Terra Mission," Proceedings of the International Symposium on Space Dynamics, CNES, June 26-30, 2000
2. C. Gramling, A. Long, and G. Horstkamp, "Autonomous Navigation Integrated with Spacecraft Communication Systems," paper AAS 96-003, presented at the AAS Guidance and Control Conference, Breckenridge, Colorado, February 7-11, 1996
3. R. Hart, A. Long, and T. Lee, "Autonomous Navigation of the SSTI/Lewis Spacecraft Using the Global Positioning System (GPS), Proceedings of the Flight Mechanics Symposium 1997, NASA Conference Publication 3345, May 19-21, 1997, p. 123-133
4. D. Folta et al., "Autonomous Navigation Using Celestial Objects," paper AAS 99-439 presented at the AAS/AIAA Astrodynamics Specialist Conference, Girdwood, Alaska, August 16-19, 1999
5. Goddard Space Flight Center, Flight Dynamics Division, CSC-96-932-05ROUDO, Global Positioning System (GPS) Enhanced Orbit Determination (GEODE) Mathematical Specifications Version 4, T. Lee and A. C. Long, prepared by Computer Sciences Corporation, January 1999
6. Computer Sciences Corporation, CSC-86-910-18, Spacecraft Attitude Determination Accuracy From Mission Experience Revision 1 Update 1, J. Hashmall, D. Brasaveanu, and N. Ottenstein, October 1999
7. S. Nordine et al., "DIODE: Determination Immediate D'Orbite Par DORIS Embarque Software Improvements Since SPOT4 Demonstration Mission," Proceedings of the International Symposium on Space Dynamics, CNES, June 26-30, 2000