Optimal attitude corrections for cylindrical spacecraft

Advances in Space Research

Volumn 31, Issue 8, 2003, Pages 1987-1993

  Zanardi, M C ^a   Santos, R M K ^a   da Silva Fernandes, S ^b  

^a SÃO PAULO STATE UNIVERSITY UNESP   (Brazil)

^b INSTITUTO TECNOLÓGICO DE AERONÁUTICA   (Brazil)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; BOUNDARY VALUE PROBLEMS; HAMILTONIANS; OPTIMAL CONTROL SYSTEMS; ORBITS; PROBLEM SOLVING; SATELLITES; TORQUE;

SHOOTING METHODS;

AEROSPACE ENGINEERING;

SPACE SHUTTLE;

EID: 0042066399     PISSN: 02731177     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0273-1177(03)00166-2     Document Type: Article

References (7)

1. Kinoshita, M., First-Order perturbations of the two finite body-problem, Publ. Astron. Soc. Japan, 24, 423-457, 1972.
2. Lum, K.Y., and A. M. Bloch, Generalized Serret-Andoyer transformation and applications for controlled rigid body, Dynamic and Control, 9, 39-66, 1999.
3. Pontryagin, L.S., V.G. Boltyanskii, R.V. Gamkrelefge, and E.F. Mishchenko, The Mathematical Theory of Optimal Processes, John Wiley and Sons, New York, 1962.
4. Santos, R.M.K., S. Da Silva Fernandes, and M.C. Zanardi, A linear solution for the artificial satellite's attitude optimal control, RBCM - Journal of the Brazilian Society of Mechanics Sciences, Special Issue, 565-578, 1999.
5. Santos, R.M.K., Otimização do Controle da Atitude de Satélites Artificiais, Doctoral Thesis, Aeronautical Technologic Institute, São José dos Campos, São Paulo, Brazil, 2000.
6. Zanardi, M. C., and Vilhena de Moraes, R., Analytical and semi-analytical analysis of an artificial satellite's rotational motion, Cel. Mech. and Dyn. Astr., 75, 227-250, 1999.
7. Zanardi, M. C., Santos, R. M. K. and Da Silva Fernandes, S., Optimal attitude control of an artificial satellite with spherical symmetry using Andoyer variables, in Proceeding of the International Symposium on Space Flight Dynamics, Biarritz, France, 2000.