Citation

Abstract

This article discusses the potential application of the dual spacecraft tracking technique to the Voyager mission. First, the concept and technology status is reviewed briefly. Then results pertaining to the JSX-Uranus option Saturn encounter, where potential navigation benefits are greatest, are presented. Results for a Jupiter encounter demonstration also are given and, finally, software modifications and tracking requirements are discussed.

Details

Volume
42-43
Published
February 15, 1978
Pages
82–89
File Size
691.8 KB