Student nanosatellite development: From passive stabilization to three-axis active attitude control

Advances in the Astronautical Sciences

Volumn 133, Issue , 2009, Pages 597-606

  Brak, Stefan ^a   Amini, Rouzbeh ^a   Massioni, Paolo ^b  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ADVANCED TECHNOLOGY; ATTITUDE DETERMINATION AND CONTROL SYSTEM; ATTITUDE MANEUVER; ATTITUDE SENSORS; BI-DIRECTIONAL; FLIGHT EXPERIMENTS; GROUND STATIONS; HIGHLY INTEGRATED; MAGNETORQUERS; MATLAB /SIMULINK; MEASUREMENT DATA; MICRO PROPULSION; NANOSATELLITE; OPERATION MODE; PASSIVE STABILIZATION; POINTING ACCURACY; REACTION WHEELS; SENSOR AND ACTUATORS; STABILIZING CONTROL; SUN SENSOR; THREE-AXIS;

ACTUATORS; ATTITUDE CONTROL; COMPUTER SIMULATION; CONTROL SYSTEMS; SENSORS;

FLIGHT CONTROL SYSTEMS;

EID: 80053433622     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

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7. Wertz, J.R., "Spacecraft Attitude Determination and Control", Computer Sciences Corporation, Kluwer Academic Publishers, Dordrecht, 1978.
8. Wie, B., Weiss, H., Arapostathis, A., "Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations", Journal of Guidance, Control and Dynamics, Vol. 12, no. 3, 1989.