SPECIAL PERTURBATIONS WEIGHTED DIFFERENTIAL CORRECTION PROGRAM DOCUMENT
Abstract
A computer program is described which differentially corrects and/or predicts the orbit of a geocentric satellite. The dynamics of the program are based on a variation of parameters formulation with the perturbative acceleration being numerically integrated. A weighted correction process is incorporated which considers the relative accuracy of the observational data in a least-squares fit. Included in the document are the program description, complete formulation, program operating instructions, flow diagrams, and test cases.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 11, 1963
- Accession Number
- AD0426035
Entities
People
- J. D. Enright
- M. J. Kruger