Estimating attitude from vector observations using a genetic algorithm-embedded quaternion particle filter

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

Volumn 5, Issue , 2004, Pages 2983-3006

  Oshman, Yaakov ^a,b   Carmi, Avishy ^a,b  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b Department of Aerospace Engineering ^*  (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; ESTIMATION; FLIGHT DYNAMICS; GEOMAGNETISM; KALMAN FILTERING; MAGNETOMETERS; MATRIX ALGEBRA; MONTE CARLO METHODS; PROBABILITY DENSITY FUNCTION; RANDOM PROCESSES; SPACECRAFT; STATISTICAL METHODS; VECTORS;

LOW EARTH ORBIT (LEO); QUATERNION PARTICLE FILTER; SEQUENTIAL MONTE CARLO (SMC); THREE-AXIS MAGNETOMETER (TAM);

GENETIC ALGORITHMS;

EID: 19944422777     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5340     Document Type: Conference Paper

References (11)

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3. Bar-Itzhack, I. Y. and Oshman, Y., "Attitude Determination from Vector Observations: Quaternion Estimation," IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-21, No. 1, Jan. 1985, pp. 128-136.
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9. A. Kong, J. L. and Wong, W., "Sequential Imputations and Bayesian Missing Data Problems," Am. Stat. Assoc., Vol. 89, No. 425, 1994, pp. 278-288.
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11. Shiryaev, A., Waller, R., Roznov, M., and Guelman, M., "Design And Experimental Testing of Three-Axis Satellite Attitude Control Systems That Use Only Magnetic Torquers," Tech. Rep. 2002.07, Norman and Helen Asher Space Research Institute, Technion - Israel Institute of Technology, June 2002.