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Gary MKIII University of Central Florida Chris Valle, Braden Urban, John Rowe, and Tyler Yoemans.

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Presentation on theme: "Gary MKIII University of Central Florida Chris Valle, Braden Urban, John Rowe, and Tyler Yoemans."— Presentation transcript:

1 Gary MKIII University of Central Florida Chris Valle, Braden Urban, John Rowe, and Tyler Yoemans

2 Mission Collect and transmit temperature, pressure, and altitude data, as well as take a picture at 80,000 feet. – Use temperature data to activate and turn off heaters, ensuring the interior of the box is kept above 10 degrees Celsius. – Use pressure data to estimate altitude using function stored in computer, and activate camera at desired altitude. – Use the power distribution board in conjunction with the computer to activate and turn off components. – Transmit data to ground with radio, as well as store it on onboard SD Card.

3 SHOT II / UN-4 Connection: The purpose of the payload it to test Power and C&DH flight hardware, as well as provide the team an opportunity to practice programming.

4 Communications Two Kenwood TH-D7A radios Proof of concept. We are able to transmit data from the computer on a relatively low frequency band. Box antenna consists of just the radio. Ground station consists of radio connected to a Yagi antenna. Weather Balloon BoxGround Station Powered by the on-board power system. Powered by stock battery pack. Transmit OnlyReceive Only Communicates using our Atmel powered board. Communicates using a laptop running Hyper Terminal.

5 Power Distribution Power provided by six 9-Volt batteries in parallel. Regulated by two AP34063 Universal DC to DC converters – One chip to reduce 5 volts for computer – The other to boost to 13.8 for the radio Power control based off of MOSFETs, switched on and off by computer.

6 C&DH EVK1100 development kit – This kit comes equipped with the 32-bit ATMEL processor which Knightsat’s C&DH was designed around Comm. Interfaced via RS-232 USART0 Camera interfaced via RS-232 USART2 Pressure and temperature sensors interfaced through 6 of the 8 ADC channels Using the multiplexer on our GPIO we are able to use unmapped pins to provide a 3.3V signal to trigger the MOSFETs

7 Test Program and Compliance Individual testing of each component Integration of two, three, then all systems Payload complies with all User’s guide requirements for: – Center of mass – Total mass – Communication bandwidth restrictions – Integration with flight string

8 Expected Results Temperature, Pressure, and Altitude data will be transmitted to ground All data and photograph will be stored to onboard memory – Data is expected to show that correct temperatures were maintained, image was taken at the correct altitude, and that all systems were activated at the correct times.

9 Demonstration Send Data over the radios Demonstrate power control


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