The Hyperbolic Kepler's Equation, and the Elliptic Equation Revisited
Abstract
A procedure is developed that, in two iterations, solves the hyperbolic Kepler's equation in a very efficient manner, and to an accuracy that proves to be always better than 10 to the minus 20th power (relative truncation error). Earlier work on the elliptic equation has been extended by the development of a new procedure that solves to a maximum relative error of 10 to the minus 14th power. Keywords: Great Britain.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1989
- Accession Number
- ADA213663
Entities
People
- A. W. Odell
- Robert H. Gooding
Organizations
- Royal Aircraft Establishment