Simple orbit determination using GPS based on a least-squares algorithm employing sequential Givens rotations

DOI10.1155/2007/49781zbMath1165.70002OpenAlexW1981083015MaRDI QIDQ954561

Aurea Aparecida da Silva, Rodolpho Vilhena de Moraes, Hélio Koiti Kuga

Publication date: 24 November 2008

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://eudml.org/doc/55792

zbMATH Keywords

JGM-2 gravity field modelTOPEX/POSEIDON satellite

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Celestial mechanics (70F15) Orbital mechanics (70M20)

Cites Work

• Factorization methods for discrete sequential estimation
• Computation of Plain Unitary Rotations Transforming a General Matrix to Triangular Form
• Recursion formulas of Legendre functions for use with nonsingular geopotential models
• Uniform Representation of the Gravitational Potential and its Derivatives
• Unitary Triangularization of a Nonsymmetric Matrix
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