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Payload transmitter unit

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dc.contributor.author Razzaq, Muhammad Ahsan
dc.contributor.author Khan, Mohammad Omer
dc.contributor.author Khan, Sherbaz Omar
dc.contributor.author Supervised by Asst Prof Engr Fazal Ahmed
dc.date.accessioned 2020-11-03T07:51:10Z
dc.date.available 2020-11-03T07:51:10Z
dc.date.issued 2015-05
dc.identifier.other PTC-260
dc.identifier.other TCC-23
dc.identifier.uri http://10.250.8.41:8080/xmlui/handle/123456789/8833
dc.description.abstract The payload transmitter unit is primarily the living brain of a satellite and comprises of several small modules. Initially, it was accepted as part of PNSS-1 from SUPARCO but, due to delay in funding instead of space/military grade components, normal off the shelf low cost components have been utilized to achieve almost the same results as envisaged through PNSS-1. It consists of transceiver and is capable of receiving the control signal from ground station transmitter on the basis of which it transmits all telemetry information i.e. temperature, current and humidity to ground station employing BPSK modulation at data rate of 256Kbps. In addition it is capable of receiving frequency modulated voice/audio signal from ground station and retransmit at another frequency of 110MHz to the ground station. In order to incorporate the telemetry information in the payload transmitter, only temperature sensor and one humidity sensor are being used along with current sensing design, interfaced through PIC microcontroller 16F877A. Arrangements have been made to display the received information on LCD device. en_US
dc.language.iso en en_US
dc.publisher MCS en_US
dc.title Payload transmitter unit en_US
dc.type Technical Report en_US


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