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

Subject Areas : Majlesi Journal of Telecommunication Devices

Mohammad Reza Jalali ¹ , Majid Tavanpour ² , Mojtaba Tavanpour ³

1 - professor
2 -
3 -

Received: 2019-03-08 Accepted : 2019-03-11 Published : 2019-06-01

Keywords:

References:

[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.