NDLI: Design and navigation control of an advanced level CANSAT

Content Provider	IEEE Xplore Digital Library
Author	Celebi, M. Ay, S. Ibrahim, M.K. Aydemir, M.E. Bensaada, M. Fernando, L.H.J.D.K. Akiyama, H. Yamaura, S.
Copyright Year	2011
Description	Author affiliation: Technical Space Center, 01 Avenue de la Palestine BP13 31200, Arzew Oran, Algeria (Bensaada, M.) \|\| Aerospace Engineering Department, Faculty of Engineering, Cairo University, Giza 12613, Egypt (Ibrahim, M.K.) \|\| Institute for Education on Space, Wakayama University, 640-8510, Japan (Akiyama, H.; Yamaura, S.) \|\| Department of Aerospace Engineering, Turkish Air Force Academy 34149, Yeşilyurt, Istanbul, Turkey (Celebi, M.; Ay, S.) \|\| Department of Electronics Engineering, Turkish Air Force Academy 34149, Yesilyurt, Istanbul, Turkey (Aydemir, M.E.) \|\| Arthur C. Clarke Institute for Modern Technologies, Katubedda, Moratuwa, Sri Lanka (Fernando, L.H.J.D.K.)
Abstract	This paper presents design and navigation control of an advanced level comeback CanSat which is going to be launched to an altitude of about 400 m using an amateur rocket from ground level. The CanSat uses advanced and ultra-light microcontroller, pressure and temperature sensors, 3-axis accelerometer, 3-axis gyro, camera, GPS, IR distance measuring sensor, and RF communication module to communicate with the ground station PC. Three actuators are considered in this work for flight and ground segments control. They are the motor driven propeller, elevator and rudder. For the flight segment, parachute and attitude control are used to control the CanSat descent rate, attitude and heading. For the ground segment control; both the propeller and the rear landing gear of the CanSat is used for heading toward a predefined location on the ground. The rear landing gear is connected to the rudder rotational axis. An indigenous navigation control and electronic circuit design with the test results also are presented in this paper.
Starting Page	752
Ending Page	757
File Size	3407829
Page Count	6
File Format	PDF
ISBN	9781424496174
e-ISBN	9781424496167
DOI	10.1109/RAST.2011.5966942
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-06-09
Publisher Place	Turkey
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Rockets Propellers Gears CanSat Navigation Control Algorithm Satellite Elevators Rocket Servomotors Launch Global Positioning System Testing
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

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