DocumentCode
752658
Title
TDRSS Performance Evaluation for Shuttle Services Using Analytical Simulation
Author
Lindsey, William C. ; Braun, Walter R.
Author_Institution
University of Southern California, Los Angeles, CA, USA
Volume
26
Issue
11
fYear
1978
fDate
11/1/1978 12:00:00 AM
Firstpage
1723
Lastpage
1731
Abstract
An analytical simulation package called LinCsim has been developed by LinCom Corporation for analytical verification of bit error rate and tracking service performance for both
- and
-band Shuttle user service through the Tracking and Data Relay Satellite System (TDRSS). The purpose of this effort was to provide a tool to assess overall system performances as well as the sensitivity to key subsystem parameters and to ensure compatibility of TDRSS and Shuttle transponder performance specifications. The evaluation is based on an analytical simulation, i.e., a combination of simulation techniques and analytical performance evaluation. This allows the use of a more realistic signal format than is possible with a purely analytical approach and maintains the advantage of short computation time. The Shuttle forward and return link models and the main features of the simulation are described. Sample results of the computer runs are provided for current power budgets and system design parameters.
- and
-band Shuttle user service through the Tracking and Data Relay Satellite System (TDRSS). The purpose of this effort was to provide a tool to assess overall system performances as well as the sensitivity to key subsystem parameters and to ensure compatibility of TDRSS and Shuttle transponder performance specifications. The evaluation is based on an analytical simulation, i.e., a combination of simulation techniques and analytical performance evaluation. This allows the use of a more realistic signal format than is possible with a purely analytical approach and maintains the advantage of short computation time. The Shuttle forward and return link models and the main features of the simulation are described. Sample results of the computer runs are provided for current power budgets and system design parameters.Keywords
Satellite telemetry; Space Shuttle; Space-vehicle communications; Analytical models; Bit error rate; Computational modeling; Packaging; Performance analysis; Power system modeling; Relays; Satellites; Signal analysis; Transponders;
fLanguage
English
Journal_Title
Communications, IEEE Transactions on
Publisher
ieee
ISSN
0090-6778
Type
jour
DOI
10.1109/TCOM.1978.1094015
Filename
1094015
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