| タイトル | Amplitude steered array |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740012747 |
| 著者（英） | Koloboff, G. J.; Johnson, C. C.; Dietrich, F. J.; Martel, R. J. |
| 著者所属（英） | NASA Goddard Space Flight Center|Westinghouse Electric Corp.|Philco-Ford Corp. |
| 発行日 | 1974-04-23 |
| 言語 | eng |
| 内容記述 | A spin stabilized satellite has an electronically despun antenna array comprising a multiplicity of peripheral antenna elements. A high gain energy beam is established by connecting a suitable fraction or array of the elements in phase. The beam is steered or caused to scan by switching elements in sequence into one end of the array as elements at the other end of the array are switched out. The switching transients normally associated with such steering are avoided by an amplitude control system. Instead of abruptly switching from one element to the next, a fixed value of power is gradually transferred from the element at the trailing edge of the array to the element next to the leading edge. |
| NASA分類 | THERMODYNAMICS AND COMBUSTION |
| レポートNO | 74N20860 |
| 権利 | No Copyright |
