Knowledge (XXG)

ITUpSAT1

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Design of a deployable antenna system for a CubeSat, after investigating of various alternatives. The pin mechanism selected includes bases to attach the antennas and pins to wrap them around. The pins and bases are attached to the solar panels with small screws. The cables are routed to a connector
386:(USB) port and external power supply connector. Also an interface to MHX series radio modems from Microhard Systems is available on the flight module. The FM430 is equipped with an MSP430F1611 microcontroller, a 16 bit 8 MHz low power microcontroller from 615:
magnet. The magnetometer will help to counter the inherent bias and drifts of inertial sensors and provide measurement updates for a filtered and corrected solution of the attitude. The analog-digital conversion of all the sensor outputs is done by a
390:. It has many peripherals such as I2C (Inter-Integrated Communication), SPI (Serial Peripheral Interface), UART (Universal Asynchronous Receiver/Transmitter) buses, and also supports DMA (Direct Memory Access). It has a flash memory of 55 433:
In addition, ITUpSat-1 features a beacon for easy identification and continuous reporting of critical telemetry. Unlike the other transceiver, it always be on during the orbit, and be transmitting identification and simple telemetry in
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was built at the ITU for the operations (monitoring and control services) of ITUpSat-1. The MHX modem (Microhard Systems) is also installed in the ground station for communication with the satellite's nominal communication system.
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with a detector array of 640 x 480 pixels (COTS imager based on the OV7620 image sensor). The objective is to take snapshot imagery. An interface board is designed to integrate camera with the MSP430F1611 microcontroller.
442:) every two minutes. This means anyone with the knowledge of the orbital parameters (in particular the amateur radio community) can easily pick up the satellite's signal. The beacon has a 100 mW RF output capacity. 365:
The electrical power subsystem consists of face-mounted solar panels, a regulator board and associated batteries. The system is able to charge itself (maximum power point tracking) and provide a regulated 3.3
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in India, and became the first Turkish university satellite to orbit the Earth. It was expected to have a minimum of six-month life term, but it is still functioning for over two years. It is a
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material (CubeSat Kit by Pumpkin Inc.). There are three identical side faces and one face with access ports. The spacecraft stabilisation concept is discussed under Payload.
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The overall objectives are to provide a hands-on project environment for the students at the ITU under faculty guidance. The mission goals are to capture imagery of the
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The FM430 flight module of Pumpkin Inc. is being used. The FM430 is a compact solution for harsh environment systems. It has an SD (Secure Digital) card interface, one
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The primary on-board communication system is the MHX-425 transceiver from Microhard Systems. This frequency hopping spread spectrum radio, which works in the
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This subsystem represents the attitude sensing and passive stability hardware. It consists of three gyros, a three-axis accelerometer both from
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modulation), the data rate is 19.2 kbit/s. The transceiver interfaces directly to the on-board computer, it has a mass of about 80 gram.
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are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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of ISRO (Indian Space Research Organisation) with a launch mass of 960 kg. Further secondary payloads on this flight were:
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
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microprocessor which also has the task of grouping the measurements into a packet and sending them over the
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with side lengths of 10 centimetres (3.9 in) and a mass of 0.990 kilograms (2.18 lb).
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ITUpSat-1 was launched on 23 September 2009 as a secondary payload atop a PSLV launcher of
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payload, and to study the behavior of the passive stabilisation system of the CubeSat.
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representing the uppermost circuit of the electronics stack of the satellite.
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The CubeSat features two payloads. The first one is a sensor suite with an
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98.50 minutes, the local equatorial crossing time is at 12:00 hours.
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near circular orbit at altitude of 720 kilometres (450 mi),
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band has adjustable hopping patterns, a high sensitivity (-115
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The spacecraft structure was purchased from Pumpkin Inc. of
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bus to the on-board computer for downlink transmission.
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Center for Satellite Communications and Remote Sensing
770:İTÜ Uçak ve Uzay Bilimleri Fakültesi TA1KS ITUPSAT-1 2411: 2370: 2351: 2314: 2269: 2220: 2179: 2149: 2124: 2110: 2094: 2065: 2049: 2027: 2006: 1995: 1877: 1861: 1841: 1820: 1792: 1764: 1672: 1644: 1637: 1525: 1449: 1405: 1301: 1249: 1148: 1113: 1038: 983: 938: 871: 829: 264: 254: 244: 234: 224: 214: 204: 199: 181: 167: 156: 148: 143: 127: 119: 114: 98: 88: 75: 54: 40: 30: 506:(University of Würzburg Experimentalsatellit-2), 2207:National Center for High Performance Computing 761:, ITU Space Systems Design and Test Laboratory 303:. It was launched on 23 September 2009 atop a 1971: 1849:BKZS (Regional Positioning and Timing System) 1615: 790: 289:Istanbul Technical University picoSatellite-1 8: 21: 2212:TRIGA Mark-II Training and Research Reactor 2003: 1978: 1964: 1956: 1641: 1622: 1608: 1600: 797: 783: 775: 607:in addition to a three-axis magnetometer ( 66: 20: 583:, and the second one is a low-resolution 640:The camera can be operated in VGA/QVGA ( 518:École Polytechnique Fédérale de Lausanne 398:. The microcontroller unit consumes 100 374:outside for connection to the antennas. 698: 297:Faculty of Aeronautics and Astronautics 45:Faculty of Aeronautics and Astronautics 2507:Earth observation satellites of Turkey 2160:Earth Sciences (Eurasia Institute of) 7: 2459: 2172:Advanced Studies in Music Department 93:http://usl.itu.edu.tr/usl.itu.edu.tr 2512:Spacecraft launched by PSLV rockets 2202:Fuat Kulunk High Voltage Laboratory 2363:ITU Hornets American football team 2331:Natural History and Science Museum 186:Indian Space Research Organisation 14: 2137:Turkish Music State Conservatory 2102:Naval Architecture and Ocean Eng. 2458: 2447: 2446: 2322:Suleyman Demirel Cultural Center 671: 2132:Textile Technologies and Design 2034:Chemical and Metallurgical Eng. 632:Payload #2 is a low-resolution 591:and are physically on the same 418:), and output power of up to 1 2057:Electrical and Electronic Eng. 730:"İstanbul Teknik Üniversitesi" 687:Polar Satellite Launch Vehicle 307:satellite launch vehicle from 78: 1: 2487:Istanbul Technical University 2252:Mühendishane-i Berr-i Hümayun 2247:Mühendishane-i Bahr-i Hümayun 2042:Computer and Informatics Eng. 1988:Istanbul Technical University 494:Technische Universität Berlin 301:Istanbul Technical University 49:Istanbul Technical University 646:Quarter Video Graphics Array 2502:Spacecraft launched in 2009 587:. The two payloads share a 2528: 1937: 475:Satish Dhawan Space Centre 361:Electrical power subsystem 309:Satish Dhawan Space Centre 2442: 2125:  T   2111:  S   2095:  N   2066:  M   2050:  E   2028:  C   2007:  A   1933: 1869:UFS (Space Launch System) 1585: 278: 274: 195: 191: 139: 135: 110: 106: 26: 16:Turkish CubeSat satellite 1910:Roketsan Research Center 1339:Universitetsky-Tatyana-2 2262:Yüksek Mühendis Mektebi 2259:Mühendis Mekteb-i Alisi 1631:Space program of Turkey 710:. Jonathan's Space Page 465:The launch site is the 2394:ITU in popular culture 2388:ITU Alumni Association 2169:Science and Technology 370:and 5 V bus service. 205:Reference system 115:Spacecraft properties 2327:Mustafa Inan Library 813:Orbital launches in 706:McDowell, Jonathan. 642:Video Graphics Array 384:Universal Serial Bus 2359:ITU basketball team 2117:Science and Letters 1944:Turksat (satellite) 736:on 21 February 2010 708:"Satellite Catalog" 23: 2492:Student satellites 2198:Central Laboratory 679:Spaceflight portal 534:nanosatellites of 402:of power at most. 394:and 10 kB of 270:23 September 2009 200:Orbital parameters 2474: 2473: 2256:Hendese-i Mülkiye 2145: 2144: 1953: 1952: 1940:Türksat (company) 1857: 1856: 1766:Earth observation 1597: 1596: 571:Sensor complement 406:RF communications 388:Texas Instruments 378:On-board computer 282: 281: 152:23 September 2009 35:Earth observation 2519: 2466: 2462: 2461: 2454: 2450: 2449: 2371:Life and culture 2281:Ayazağa (Maslak) 2273: 2224: 2183: 2153: 2004: 1999: 1989: 1980: 1973: 1966: 1957: 1642: 1624: 1617: 1610: 1601: 1001:Kwangmyŏngsŏng-2 818: 817: 816: 799: 792: 785: 776: 765:ITUpSAT1 Gallery 746: 745: 743: 741: 732:. Archived from 726: 720: 719: 717: 715: 703: 681: 676: 675: 674: 346:, consisting of 226:Perigee altitude 144:Start of mission 99:Mission duration 80: 71: 70: 64: 24: 2527: 2526: 2522: 2521: 2520: 2518: 2517: 2516: 2477: 2476: 2475: 2470: 2464: 2452: 2438: 2424:RV MTA Sismik 1 2407: 2366: 2347: 2310: 2271: 2265: 2222: 2216: 2191:Arı Technopolis 2181: 2175: 2151: 2141: 2120: 2106: 2090: 2081:Mechanical Eng. 2061: 2045: 2023: 1997: 1991: 1987: 1984: 1954: 1949: 1946: 1929: 1873: 1853: 1837: 1816: 1788: 1760: 1668: 1633: 1628: 1598: 1593: 1588: 1581: 1521: 1466:Progress M-MIM2 1445: 1401: 1297: 1245: 1144: 1109: 1034: 979: 934: 867: 825: 824: 814: 812: 811: 809: 803: 755: 750: 749: 739: 737: 728: 727: 723: 713: 711: 705: 704: 700: 695: 677: 672: 670: 667: 654: 630: 601: 589:microcontroller 573: 568: 552:Sun-synchronous 549: 516:, a CubeSat of 462:, Netherlands. 448: 408: 380: 363: 336: 236:Apogee altitude 219:Sun-synchronous 65: 60: 17: 12: 11: 5: 2525: 2523: 2515: 2514: 2509: 2504: 2499: 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2019:Architecture 1885:TÜBİTAK UZAY 1878:Institutions 1653: 1589: 1571:Soyuz TMA-17 1569: 1480: 1396:Soyuz TMA-16 1394: 1368: 1280: 1178: 1104:Soyuz TMA-15 1102: 1055: 991:Eutelsat W2A 974:Soyuz TMA-14 972: 950: 898:Ekspress-MD1 740:24 September 738:. 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Index

Earth observation
Faculty of Aeronautics and Astronautics
Istanbul Technical University
COSPAR ID
2009-051E
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SATCAT no.
http://usl.itu.edu.tr/usl.itu.edu.tr
PSLV
Satish Dhawan
FLP
Indian Space Research Organisation
Geocentric
Sun-synchronous
Perigee altitude
Apogee altitude
Inclination
Period
Epoch
CubeSat
Faculty of Aeronautics and Astronautics
Istanbul Technical University
PSLV-C14
Satish Dhawan Space Centre
Sriharikota
Andhra Pradesh
picosatellite
CMOS
San Francisco
California

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