DocumentCode
3277250
Title
“TSIKADA-M-UTTH” multi-purposes satellite system
Author
Cheremisin, K. ; Kosenko, V. ; Zvonar, V. ; Chebotarev, K.
Author_Institution
NPO PM, Krasnoyarsk, Russia
Volume
2
fYear
1994
fDate
18-21 Oct 1994
Firstpage
204
Abstract
The TSK multi-purpose satellite system has been developed to replace first generation low-orbit navigation systems as well as the COSPAS-SARSAT system. The system will provide operations for both existing customers and new customers having advanced equipment. TSK is to perform the following tasks: definition of the location of an unlimited number of mobile customers in any region of the globe independently of weather; maritime vehicles and aeroplanes location definition in an emergency; support the ELECON-STIR system: consignment monitoring and traffic control. The orbital constellation consists of seven satellites which are located within seven orbital planes equally distributed along the equator in longitude (circular orbit height is about 1,000 km; orbit inclination is 83 ang. degrees). This provides for customers to be in touch with the satellite on average for 90 minutes in equatorial regions, 45 minutes at mid-latitudes, and 20 minutes at high geographical latitudes
Keywords
aircraft navigation; satellite navigation; ships; COSPAS-SARSAT; ELECON-STIR system; TSIKADA-M-UTTH; TSK; aeroplanes; consignment monitoring; emergency; location; low-orbital navigation systems; maritime vehicles; mobile customers; multi-purposes satellite system; orbital constellation; traffic control; Artificial satellites; Data processing; Extraterrestrial measurements; Force measurement; Frequency; Monitoring; Satellite navigation systems; Timing; Traffic control; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Satellite Communications, 1994. ICSC'94., Proceedings of International Conference on
Conference_Location
Moscow
Print_ISBN
0-7803-2514-1
Type
conf
DOI
10.1109/ICSC.1994.523165
Filename
523165
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