Effects of navigation filter properties on formation flying control

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 2, Issue , 2004, Pages 1464-1476

  Mitchell, Megan ^a   Breger, Louis ^a   How, Jonathan P ^a   Alfriend, Kyle T ^b  

^a Massachusetts Institute of Technology Cambridge   (United States)

^b TEXAS A AND M UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AIR NAVIGATION; COMPUTER SIMULATION; CORRELATION METHODS; ERRORS; ESTIMATION; GLOBAL POSITIONING SYSTEM; KALMAN FILTERING; MATHEMATICAL MODELS; SENSORS; SPACECRAFT;

CARRIER-PHASE DIFFERENTIAL GPS (CDGPS); CONTROL DESIGN; CORRELATION COEFFICIENTS; LINEAR PLANAR MODEL;

FLIGHT DYNAMICS;

EID: 19644364343     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5024     Document Type: Conference Paper

References (11)

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9. M. Grewal, A. Andrews. Kalman Filtering. Wiley, 2001.
10. F. Busse, "Precise Formation-State Estimation in Low Earth Orbit Using Carrier Differential GPS," Ph.D. Dissertation, Stanford University, Dept. Aeronautics and Astronautics. Feb. 2003.
11. F. D. Busse, J. Simpson, and J. P. How, "Demonstration of Adaptive Extended Kalman Filtering for LEO Formation Estimation Using CDGPS," Navigation Journal of the Institute of Navigation, Vol. 50, No. 2, Summer 2003, pp. 79-94.