ANTENNA POINTING REQUIREMENTS FOR SATELLITE TRACKING.
Abstract
In order to determine the satellite tracking capability of an azimuth-elevation antenna mount, a simplified model for satellite motion is presented. Satellite azimuth and elevation positional equations versus time are derived and the results of a computer program to determine velocity and acceleration are presented in both tabular and graphical forms. In terms of the results obtained the satellite tracking performance of the AFCRL 29-Foot Millimeter Wave Antenna is evaluated. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1966
- Accession Number
- AD0634155
Entities
People
- Joseph A. Short Jr
Organizations
- Air Force Cambridge Research Laboratories