iet.ntnu.no

q2s.ntnu.no

Partners - Q2S Centre of Excellence Archive

http://q2s.ntnu.no/partners

Skip to local navigation. Skip to global navigation. Norwegian University of Science and Technology. Search in NTNU website. NTNU, Dept. of Telematics. NTNU, Dept of Electronics and Telecommunications. Where to find us. 2011/01/14 13:31, Hans Almåsbakk. Visiting address: Gamle fysikk, 3. etasje, Sem Sælands vei 5, Gløshaugen, 7034 Trondheim. Phone: 47 73 59 42 02 Fax: 47 73 59 36 28 E-mail: postmottak@ime.ntnu.no. NTNU, NO-7491 Trondheim. Telephone: 47 73 59 50 00. Contact us.

nuts.cubesat.no

The satellite - NUTS

http://nuts.cubesat.no/the-satellite

The mechanical system comprises all components of the satellite with a mass and volume, i.e. everything that isn't software. This ranges from the location and fixation of the batteries to the thickness, design and manufacturing of carbon fiber panels for the frame. The biggest challenge so far has been to design a structure that can withstand heavy loads, be reliable in space and have a reasonably simple manufacturing process. The Attitude Determination and Control System (ADCS) is responsible for adjust...

nuts.cubesat.no

OBC - NUTS

http://nuts.cubesat.no/obc

The On-Board Computer will provide computing power for the payload, as well as log events, issue commands to the other modules in the satellite and monitor the state of the whole system. It is also one of the backplane master modules, meaning it is able to control certain aspects of the backplane, as described in the backplane section. Command scheduling and dispatching. 128KB SRAM and 256KB flash/program memory integrated in MCU package. 16Mbit SRAM external to MCU. Operating system: FreeRTOS 7.

nuts.cubesat.no

Ground Station - NUTS

http://nuts.cubesat.no/ground-station

We now have the ground station partly operational. So far, we only got access to polarization, but during summer and autoumn, we will mount equipment to gain access to the other polarization alternatives also. We have one antenna mast with tracking capabilities with UHF and VHF yagi antennae. In addition, we have a "mobile" turnsitle antenna for weather satellite (NOAA) data reception. Our antenna mast with antennae. Equipment for main ground station. Tonna 2x9 crossed Yagi-Uda for VHF. If you'd like to ...

balasingham.com

Dr. Ilangko Balasingham

http://www.balasingham.com/page2.html

I was born in Jaffna, Sri Lanka and left to Norway in 1985 due to civil war. I received the Siv.Ing (MSc) and Dr.Ing. (PhD) degrees both in signal processing from the Signal Processing Group. Department of Electronics and Telecommunications. Norwegian University of Science and Technology. Oslo University Hospital - Rikshospitalet. My research interests include medical signal and image processing, wireless biomedical sensor networks for short range sensing, imaging, localization and communication, and mul...

nuts.cubesat.no

New students - NUTS

http://nuts.cubesat.no/new-students

Do you want to join us? Criterions to join NUTS. In order to join the NUTS project you must be a student enrolled at NTNU and preferably have a keen interest in space technology. By joining the team you must be able to take responsibility and see to it that you are fully dedicated to the task you have been handed. Your commitment to the project and the other team members obligates you to work 4-5 hours each week on project related tasks. Available positions in the team. Project manager Roger Birkeland.

nuts.cubesat.no

Om - NUTS

http://nuts.cubesat.no/om

NUTS - NTNU Test Satellite. The NTNU Test Satellite (NUTS) project is organized and supported by the Department of Electronics and Telecommunications (IET) at NTNU. The aim of this project is to design, build, test and launch a double CubeSat by 2016. NUTS is part of the Norwegian Student Satellite Program (ANSAT), which is managed by NAROM. For more information on the organizers of NUTS please visit ORGANIZER. Deliver a tested satellite according to mission specifications. Test the payload camera. Test ...

nuts.cubesat.no

Mechanical - NUTS

http://nuts.cubesat.no/mechanical

The current frame is a vowen CRFP-based (Carbon Fibre Reinforced Plastic) epoxy structure, which gives us a good strength to weight ratio and an unique frame solution which has never been used on a CubeSat before. We're also testing a brand new and as-of-yet untested technique for bonding the solar cells themselves to the frame by using BGA soldering instead of the usual glue-based mounting solutions. Project manager Roger Birkeland. Satellitte lab: Room D551. Webdesign og webutvikling: InCreo.

nuts.cubesat.no

ADCS - NUTS

http://nuts.cubesat.no/adcs

ADCS - Attitude determination and control. An attitude determination and control system is important for orientation control of a satellite. An estimation method is needed for determination of the current attitude, and deviations from the expected attitude are corrected by the attitude control system. Detumbling: A dissipative controller has been explored and implemented. The preliminary simulation results are satisfactory. The choice for this controller is however still left open, as use of the ...Stabi...