Attitude control of spinning satellite subject to actuators restriction using eigenstructure assignment

1st International Symposium on Systems and Control in Aerospace and Astronautics

Volumn 2006, Issue , 2006, Pages 1413-1419

  Bolandi, H ^a   Bayat, F ^a   Nasirian, M ^b  

^a IRAN UNIVERSITY OF SCIENCE AND TECHNOLOGY   (Iran)

^b Applied Science and Research Association (ASRA)   (Iran)

Author keywords

[No Author keywords available]

Indexed keywords

DOUBLE GIMBALS SINGLE ROTOR CONTROL MOMENT GYRO (DGSR-CMG); EIGENSTRUCTURES; LOOP TRANSFER RECOVERY (LTR); SPINNING SATELLITE;

ALGORITHMS; EIGENVALUES AND EIGENFUNCTIONS; GYROSCOPES; KALMAN FILTERING; ROTORS; SATELLITE COMMUNICATION SYSTEMS; STRUCTURES (BUILT OBJECTS);

ACTUATORS;

EID: 33750947524     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. J.M.Lin, "System Design by Linear Exponential Quadratic Gaussian and Loop Transfer Recovery Methodology", AIAA Journal of Guidance, Control and Dynamics, 1995, pp.951-958.
2. M.M.Fahamy, and O'Reilly, J., "On EigenStructure Assignment in Linear Multivariable System", IEEE Transaction on Automatic Control, AC-27, 1982, pp.690-693.
3. Marcel J.Sidi, Spacecraft Dynamics and Control, Cambridge University Press, 1997.
4. Greensite, A.L, Analysis and Design of Space Vehicle Flight Control Systems, New York Spar ton, Vol. II, 1970.
5. J.M.Maciejowski, Multivariable Feedback Design, Addition-Wesley Publishing Co., 1989, Chap.5.