Normal mode magnetic control of LEO spacecrafts, with integral action

1996 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1996, Pages 1-9

  Lagrasta, S ^a   Bordin, M ^b  

^a LEONARDO S P A   (Italy)

^b SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE CONTROL; COMMUNICATION SATELLITES; CONTROL THEORY; CONTROLLABILITY; FOURIER SERIES; HEURISTIC METHODS; MACHINERY; MAGNETIC ACTUATORS; MAGNETISM; OPTIMIZATION; SATELLITE COMMUNICATION SYSTEMS; SATELLITES; SPACECRAFT; STATE SPACE METHODS; TIME VARYING SYSTEMS; TORQUE;

CONTROLLABILITY MATRICES; FOURIER APPROXIMATIONS; HEURISTIC APPROACH; LOW EARTH ORBIT SATELLITES; MAGNETIC TORQUERS; QUASI STATIC MODELS; SATELLITE MISSION; STATE SPACE REPRESENTATION;

ORBITS;

EID: 84959076862     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

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5. W. H. Steyn. Comparison of Low- Earth-Orbit satellite attitude controllers submitted to controllability constraints, Journal of Guidance, Control and Dynamics, Vol. 17, No. 4, July-Aug. 1994, pp. 795-804.
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8. C. T. Leondes. Discrete-time dynamic and control system techniques, Vol. 66, 1994, Academic Press