메뉴 건너뛰기




Volumn 3, Issue , 2003, Pages 2383-2388

Controllability of Spacecraft Attitude Under Magnetic Actuation

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; GEOMAGNETISM; MAGNETIC FIELD EFFECTS; MATHEMATICAL MODELS; SATELLITES; SPACECRAFT; TORQUE;

EID: 1542288860     PISSN: 07431546     EISSN: 25762370     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (27)

References (16)
  • 2
    • 0021411956 scopus 로고
    • Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
    • P. E. Crouch. Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models. IEEE Tr. Aut. Contr., 29(4):321-331, 1984.
    • (1984) IEEE Tr. Aut. Contr. , vol.29 , Issue.4 , pp. 321-331
    • Crouch, P.E.1
  • 4
    • 0017542851 scopus 로고
    • Nonlinear controllability and observability
    • R. Hermann and A. J. Krener. Nonlinear controllability and observability. IEEE Tr. Aut. Contr., 22 (5): 728-740, 1977.
    • (1977) IEEE Tr. Aut. Contr. , vol.22 , Issue.5 , pp. 728-740
    • Hermann, R.1    Krener, A.J.2
  • 6
    • 0028728561 scopus 로고
    • Controllability of spacecraft systems in a central gravitational field
    • K.-Y. Lian, L.-S. Wang, and L.-C. Fu. Controllability of spacecraft systems in a central gravitational field. IEEE Tr. Aut. Contr., 39(12):2426-2441, 1994.
    • (1994) IEEE Tr. Aut. Contr. , vol.39 , Issue.12 , pp. 2426-2441
    • Lian, K.-Y.1    Wang, L.-S.2    Fu, L.-C.3
  • 7
    • 0016027128 scopus 로고
    • Controllability of nonlinear systems on compact manifolds
    • C. Lobry. Controllability of nonlinear systems on compact manifolds. SIAM J. Contr., 12:1-4, 1974.
    • (1974) SIAM J. Contr. , vol.12 , pp. 1-4
    • Lobry, C.1
  • 8
    • 0036205172 scopus 로고    scopus 로고
    • Periodic attitude control techniques for small satellites with magnetic actuators
    • M. Lovera, E. De Marchi, and S. Bittani. Periodic attitude control techniques for small satellites with magnetic actuators. IEEE Tr. Contr. Sys. Tech., 10(1):90-95, 2002.
    • (2002) IEEE Tr. Contr. Sys. Tech. , vol.10 , Issue.1 , pp. 90-95
    • Lovera, M.1    De Marchi, E.2    Bittani, S.3
  • 9
    • 0027693939 scopus 로고
    • Optimal periodic control for spacecraft pointing and attitude determination
    • M. E. Pittelkau. Optimal periodic control for spacecraft pointing and attitude determination. J. Guid. Contr. Dyn., 16(6):1078-1084, 1993.
    • (1993) J. Guid. Contr. Dyn. , vol.16 , Issue.6 , pp. 1078-1084
    • Pittelkau, M.E.1
  • 10
    • 0035278962 scopus 로고    scopus 로고
    • Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation
    • M. L. Psiaki. Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation. J. Guid. Contr. Dyn., 24(2):386-394, 2001.
    • (2001) J. Guid. Contr. Dyn. , vol.24 , Issue.2 , pp. 386-394
    • Psiaki, M.L.1
  • 11
    • 0028466155 scopus 로고
    • Comparison of low-earth-orbit satellite attitude controllers submitted to controllability constraints
    • W. H. Steyn. Comparison of low-earth-orbit satellite attitude controllers submitted to controllability constraints. J. Guid. Contr. Dyn., 17:795-804, 1994.
    • (1994) J. Guid. Contr. Dyn. , vol.17 , pp. 795-804
    • Steyn, W.H.1
  • 12
    • 84968475624 scopus 로고
    • Orbits of families of vector fields and integrability of distributions
    • H. J. Sussmann. Orbits of families of vector fields and integrability of distributions. Tr. Amer. Math. Soc., 180:171-188, 1973.
    • (1973) Tr. Amer. Math. Soc. , vol.180 , pp. 171-188
    • Sussmann, H.J.1
  • 13
    • 33144472531 scopus 로고
    • Controllability of nonlinear systems
    • H. J. Sussmann and V. Jurdjevic. Controllability of nonlinear systems. J. Diff. Eq., 12:95-116, 1972.
    • (1972) J. Diff. Eq. , vol.12 , pp. 95-116
    • Sussmann, H.J.1    Jurdjevic, V.2
  • 16
    • 0343390431 scopus 로고    scopus 로고
    • Linear time-varying approach to satellite attitude control using only electromagnetic actuation
    • R. Wieniewski. Linear time-varying approach to satellite attitude control using only electromagnetic actuation. J. Guid. Contr. Dyn., 23:640-647, 2000.
    • (2000) J. Guid. Contr. Dyn. , vol.23 , pp. 640-647
    • Wieniewski, R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.