A new procedure for the solution of the classical problem of minimal orbit determination from three lines of sight

DOI10.1007/BF00049379zbMath0900.70173OpenAlexW2071871403MaRDI QIDQ1370971

R. H. Gooding

Publication date: 30 March 1998

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00049379

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Celestial mechanics (70F15) Computational methods for problems pertaining to astronomy and astrophysics (85-08)

Related Items (5)

Dealing with uncertainties in angles-only initial orbit determination ⋮ A projective approach to orbit determination from three sight-lines ⋮ Initial orbit determination using multiple observations ⋮ Solution algorithm of a quasi-Lambert's problem with fixed flight-direction angle constraint ⋮ Parallel initial orbit determination using angles-only observation pairs

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item
• A procedure for the solution of Lambert's orbital boundary-value problem
• A projective approach to orbit determination from three sight-lines
• Procedures for solving Kepler's equation
• The hyperbolic Kepler equation (and the elliptic equation revisited)
• On universal elements, and conversion procedures to and from position and velocity
• Orbit determination by four observations

This page was built for publication: A new procedure for the solution of the classical problem of minimal orbit determination from three lines of sight