A New Design and Analysis of the Electronic Process of the Meteorological Satellite based on the Localization of Satellite Technology

Majlesi Journal of Telecommunication Devices

مقاله 7، دوره 8، شماره 2، شهریور 2019، صفحه 75-81   

نوع مقاله: Articles

نویسندگان

Mohammad Reza Jalali^* ؛ Majid Tavanpour؛ Mojtaba Tavanpour

professor

چکیده

In this research, the design and survey of the satellite (Kensett) has been addressed. The main mission is to study the atmosphere and eventually land on the air bag, and new designs and ideas were designed. The motivation for this design is to be native and affordable in comparison with foreign ones.

کلیدواژه‌ها

Meteorological Satellite؛ Localization؛ atmosphere

مراجع

[1] Bulut, S.N., Model satellite design for CanSat Competition, Published in: Recent Advances in Space Technologies (RAST), 2013 6th International Conference on; Pages 913-917, IEEE, June 2013

[2] Aydemir, M.E., Ground station design procedures for CANSAT, Published in: Recent Advances in Space Technologies (RAST), 2013 6th International Conference on; Pages 909-912, IEEE, June 2013

[3] F. Laraibi, R. Marzabadi, Numerical investigation of drag coefoicients in 2D parachute-like bodies with permeability assumption, Modares Mechanical Engineering, Vol. 15, No. 4, pp. 188-194, 2015. (in Persian)

[4] J. Cruz, C. Zumwalt, D. F. Keller, C. O’Farrell, Wind tunnel test of subscale ringsail and disk -gap-band parachutes, 34th American Institute of Aeronautics and Astronautics, Applied Aerodynamics Conference, Washington D.C., June 13-17, 2016.

[5] Bulut, S.N., Model satellite design for CanSat Competition, Published in: Recent Advances in Space Technologies (RAST), 2013 6th International Conference on; Pages 913-917, IEEE, June 2013

[6] Aydemir, M.E., Ground station design procedures for CANSAT, Published in: Recent Advances in Space Technologies (RAST), 2013 6th International Conference on; Pages 909-912, IEEE, June 2013

[7] J.-E. Pierre, R. Castellon, R. Chesneau, "CanSat: multiphysics experimental design of a probe come back mission", 9th International Planetary Probe Workshop, Toulouse, France, 16th-22nd June 2012

[8] K. Hiraki, M. Inoue, "development of autonomous flight systems with small parafoil", 20th AIAA

Aerodynamic Decelerator systems Technology Con- ference and Seminar, Seattle (US), May 2009

[9] M. Bayada, B. Lafaille, D. Le Goff, Y. Leurent, "Etude de la Pilotabilite d’un Parafoil", Engineer- ing School Student Project, Toulouse (France), June 2011

[10] A, Belnou, P. Bonijoly, X. Guihot,V. Migeon, "CanSat : Pilotage Guidage", Engineering School Student Project, Toulouse (France), June 2013

[11] N. A. Nobari, A. K. Misra, Attitude dynamics and control of satellites with fluid ring actuators, Journal of Guidance, Control and Dynamics, Vol. 35, No. 6, pp. 1855-1864, Nov-Dec 2012.

[12] J. Tayebi, A. Soleymani, A comparative study of CMG and FMC actuators for nano satellite attitude control system - pyramidal configuration, 7th International Conference on Recent Advances in Space Technologies (IEEE), Istanbul, Turkey, June 16-19, 2015.