Linear time varying approach to satellite attitude control using only electromagnetic actuation

1997 Guidance, Navigation, and Control Conference

Volumn , Issue , 1997, Pages 243-251

  Wiśniewski, Rafal ^a  

^a AALBORG UNIVERSITY   (Denmark)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE CONTROL; CONTROLLERS; GEOMAGNETISM; MAGNETIC FIELDS; RICCATI EQUATIONS; SATELLITES; TIME VARYING SYSTEMS;

ELECTROMAGNETIC ACTUATION; ELECTROMAGNETIC COILS; GEOMAGNETIC FIELD VECTORS; LOW EARTH ORBIT SATELLITES; REALISTIC ENVIRONMENTS; SATELLITE ATTITUDE CONTROL; SMALL SATELLITE MISSION; TECHNOLOGICAL IMPROVEMENTS;

ORBITS;

EID: 84959133664     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Cavallo A & al 1993, A sliding manifold approach to satellite attitude control, in 12th World Congress IFAC, Sidney.
2. Musser K & L Ward 1989, Autonomous spacecraft attitude control using magnetic torquing only, in Flight Mechanics Estimation Theory Symposium, NASA.
3. Martel F & al Sep. 1988, Active magnetic control system for gravity gradient stabilized spacecraft, in Annual AlAA/Utah State University Conference on Small Satellites.
4. Wisniewski R 1994, Nonlinear control for satellite detumbling based on magnetic torquing, in Joint Services Data Exchange for Guidance, Navigation, and Control, Arizona.
5. Wisniewski R & M Blanke Jun. 1996, Threeaxis satellite attitude control based on magnetic torquing, in 13th IFAC World Congress, San Francisco, California.
6. Wisniewski R Dec. 1996, Satellite Attitude Control Using Only Electromagnetic Actuation, Ph.D. thesis, Aalborg University.
7. Wertz J 1990, Spacecraft Attitude Determination and Control, Kluwer Academic Publishers.
8. Bittanti S, editor 1991, The Riccati Equation, Springer Verlag.
9. Kwakernaak H & R Sivan 1972, Linear Optimal Control Systems, Wiley.
10. Mohler R 1991, Nonlinear Systems, vol. Dynamics and Control, Prentice Hall.