DocumentCode
1472611
Title
Transmitter model for the design of communication satellites
Author
Ruggieri, Marina
Author_Institution
Rome Univ., Italy
Volume
35
Issue
1
fYear
1999
fDate
1/1/1999 12:00:00 AM
Firstpage
31
Lastpage
42
Abstract
The paper proposes a modeling approach for satellite communication systems able to relate analytically the on-board transmitter reliability to the effective isotropic radiated-power (EIRP) requirement. The latter, in fact, plays a key role in system design, yielding a direct impact on transmitter configuration and technological features. In addition, that requirement is directly related to the antenna characteristics and, hence, to the critical compromise between transmitter and antenna specifications. In this frame, the proposed model, which is based on an innovative design-oriented approach, is able to relate the antenna complexity to the transmitter reliability and, therefore, to the overall system reliability. The potential of the proposed approach is pointed our through the description of the analytical model and the achieved results
Keywords
design engineering; power amplifiers; radio transmitters; redundancy; reliability; satellite communication; space vehicle electronics; transmitting antennas; EIRP; analytical model; antenna characteristics; antenna complexity; antenna specifications; communication satellites; direct impact; effective isotropic radiated-power requirement; isotropic radiated-power requirement; on-board transmitter reliability; satellite communication; system design; system reliability; technological features; transmitter configuration; transmitter reliability; Analytical models; Antenna accessories; Artificial satellites; Failure analysis; Payloads; Power system modeling; Power system reliability; Solid state circuits; Transmitters; Transmitting antennas;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.745678
Filename
745678
Link To Document