Attitude determination of small spinning spacecraft using three axis magnetometer and solar panels data

IEEE Aerospace Conference Proceedings

Volumn 7, Issue , 2000, Pages 127-133

  Santoni, F ^a   Bolotti, F ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; ANGLE MEASUREMENT; COMPUTER SIMULATION; ELECTRIC CURRENT MEASUREMENT; MAGNETIC FIELDS; MAGNETOMETERS; MATHEMATICAL MODELS; SOLAR CELLS; SOLAR POWER GENERATION; SPACE FLIGHT; TEMPERATURE MEASUREMENT; VOLTAGE MEASUREMENT;

ATTITUDE DETERMINATION; DATA FILTERING; SMALL SPINNING AIRCRAFT; SOLAR PANELS; SUN ANGLE MEASUREMENT;

SATELLITE OBSERVATORIES;

EID: 0034431582     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Simple algorithm for intersecting two conical surfaces
2. Satellite attitude determination by simultaneous line-of-sight sightings