Small Perturbations on Artificial Satellites as an Inverse Problem

The geocentric motion of a satellite is mathematically simulated by a system of second order ordinary differential equations involving two perturbing functions. The first one represents the second term of the gravitational potential of the Earth and the second is due to the atmospheric drag. Assumin...

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Detalles Bibliográficos
Autor principal: Zadunaisky, P.E.
Formato: JOUR
Materias:
Taylor expansion
Computer simulation
Differential equations
Drag
Gravitational effects
Integral equations
Inverse problems
Measurement errors
Motion control
Perturbation techniques
Polynomial approximation
Vectors
Satellite communication systems
Acceso en línea:http://hdl.handle.net/20.500.12110/paper_00189251_v39_n4_p1270_Zadunaisky
Aporte de:
Biblioteca Digital - Facultad de Ciencias Exactas y Naturales (UBA) de Universidad de Buenos Aires

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