Control Aspects of Multibeam or Multielement Spacecraft Antennas

• Main Author: Foldes, Peter
• Other Authors: General Electric Company, Space Division
• Language: en_US
• Published: International Foundation for Telemetering 1979
• Online Access: http://hdl.handle.net/10150/613905; http://arizona.openrepository.com/arizona/handle/10150/613905

International Telemetering Conference Proceedings / November 19-21, 1979 / Town and Country Hotel, San Diego, California === With the rapid development of spacecraft systems the trend is toward more sophisticated and larger on-board antennas. Many of these antennas employ an array of radiating elements, either as part of a feed system illuminating a larger aperture optics or as the direct radiators. The main purpose of using multiple radiators instead of a radiator in conjunction with a large aperture is to introduce a much larger degree of freedom in achieving desirable antenna characteristics. If an antenna system contains n independent radiating elements then the amplitude and phase of each of these elements can be selected for desirable results.