DocumentCode :
246720
Title :
Multi mission low earth orbit equatorial satellite for Indonesian regions
Author :
Nasser, Eriko Nasemuddin
Author_Institution :
Satellite Technol. Center, Nat. Inst. of Aeronaut. & Space (LAPAN), Bogor, Indonesia
fYear :
2014
fDate :
13-14 Nov. 2014
Firstpage :
121
Lastpage :
126
Abstract :
Low earth orbit (LEO) equatorial satellite has become a favorable option for developing countries like Indonesia. Low propagation delay, low transmission power and also low cost in term of satellite development and launch are the main attraction of the LEO satellite system. In this paper, we propose multi mission satellite LEO equatorial satellite for telecommunication, surveillance and vessel monitoring based on AIS (Automatic Identification System). First iteration was the tradeoff between communication payload mission and other missions in defining the orbit constellation type and altitude. Simulation was done for orbit constellation, orbit environment, antenna pattern, and coverage analysis. The simulation result will become input for link budget calculation, ITU constraint (PFD and EPFD) and handover mechanism scheme selection. The result shows that single plane 1500 km LEO equatorial with 14 satellites was able to provide dual satellite diversity for all Indonesian region. It also shows that C-band and Ku-band Frequency will exceed the EPFD limit with 10 dbi antenna gain and 30 W transmit power. The optimum configuration of Ext C-band with hemispherical patch antenna shows that the minimum fading margin > 1 dB is required to implement the hard handover scheme.
Keywords :
antenna radiation patterns; artificial satellites; diversity reception; microstrip antennas; mobility management (mobile radio); radiowave propagation; satellite antennas; surveillance; AIS; C-band frequency; EPFD; Ext C-band; ITU constraint; Indonesia; Indonesian regions; Ku-band frequency; LEO satellite system; PFD; antenna pattern; automatic identification system; communication payload mission; coverage analysis; developing countries; dual satellite diversity; gain 10 dB; handover mechanism scheme selection; hemispherical patch antenna; link budget calculation; low propagation delay; low transmission power; minimum fading margin; multi mission low earth orbit equatorial satellite; orbit constellation altitude; orbit constellation type; orbit environment; power 30 W; satellite development; satellite launch; telecommunication payload; vessel monitoring; Diversity methods; Handover; Low earth orbit satellites; Orbits; Payloads; LEO Constellation; Satellite Telecommunication;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Electronics and Remote Sensing Technology (ICARES), 2014 IEEE International Conference on
Conference_Location :
Yogyakarta
Print_ISBN :
978-1-4799-6187-0
Type :
conf
DOI :
10.1109/ICARES.2014.7024394
Filename :
7024394
Link To Document :
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