Earthquake Signature Detection Using Cubesat Technology
DOI:
https://doi.org/10.53555/nneee.v1i2.256Keywords:
Cubesat, Quakesat, ELF, SSDL, Ritcher ScaleAbstract
Cubesats play a vital role in development of new micro components being used in various micro/nano satellites. Cubesats have an effective small design and have the ability to get modified easily. Quakesat, a satellite being deployed by Space Systems Development Laboratory (SSDL) is used to study, detect, record, and downlink extremely low frequency (ELF) magnetic signals, which are used to predict earthquake activity. Quakesat is a live example of cubesat technology, uses non space application components and provides a low cost alternative to launch space missions and support nano satellite infrastructure in future.
References
A.C. Fraser Smith, et. al., “Low-frequency magnetic field measurements near the epicenter of the Ms 7.1 Loma Prieta earthquake”, Geophysical Research Letters, Vol. 17, No. 9, pages 1465-1468, August 1990.
O.N. Serebryakova, et. al., “Electromagnetic ELF radiation from earthquake regions as observed by low-altitude satellites”, Geophysical Research Letters, Vol. 19, No. 2, pages 91-94, January 24, 1992.
M. Parrot, “Statistical study of ELF/VLF emissions recorded by a low-altitude satellite during seismic events”, Journal of Geophysical Research, Vol. 99, No. A12, pages 23,339-23,347, December 1, 1994.
Dallas Semiconductor, MAX1873 Li+ Charge Controller Kit, July1 2001, http://www.maximic.com/quick_view2.cfm/qv_pk/3105.
Power-One Series Single Output Power Regulator, June 2002, http://www.power-one.com/.
Wertz, J.R., and Larson, W.J., Space Mission Analysis and Design, 3rd Ed., Microcosm Press, El Segundo, CA, 1999.
Menges, B.M., Guadiamos, C.A., and Lewis, E.K., “Dynamic Modeling of Micro-Satellite Spartnik’s Attitude”, San Jose State University, http://www.engr.sjsu.edu/spartnik/adac.html.
White, J., “Microsat Motion, Stabilization, and Telemetry”, AMSAT-NA, September 1990, http://coloradosatellite.com/Papers/Motion.html.
Kim, K., “Analysis of Hysteresis for Attitude Control of a Microsatellite”, San Jose State University, http://www.engr.sjsu.edu/spartnik/adac.html.
Swartout, M., “Attitude Determination and Control, Sapphire Notes”, http://students.cec.wustl.edu/~sapphire/design/log/sec8adc/8.1.html.
Published
Issue
Section
License
This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
Terms & Condition
Submission -
Author can submit the manuscript through our online submission process or email us at the designated email id in contact details.
The other mode of submission not accepted than online and email.
Before submission please read the submission guidelines.
NN Publication accepts only article submitted in pdf/doc/docx/rtf file format. Another format except given file formats will no be considered .
Author will be responsible for the error mistakes in the submission files. The minor changes can be done without any cost after publication. But for major changes NN Publication may charges you the editing charges.
Publication (Online) -
The online publication is scheduled on last date of every month, but it can be delayed by 24 to 48 hours due to editorial process if huge number of articles comes to publish in single issue.
Automatic notificatation email will be sent to the all users on publication of an issue, so its author’s duty to check their email inbox or SPAM folder to get this notification.
After publication of article author can not withdraw their article.
If editor’s found any issue after publication of article then the NN Publication have the authority to remove the article from online website.
No refund will be provided after online publication of article.
Publication (Print) -
The print copy publication are sent as per the author’s request after 2 weeks of online publication of that issue.
NN Publication will ship the article by India Post and provide the consignment number on dispatch of print copy.
NN Publication follows all the guidelines of delivery provided by IndiaPost and hence not responsible for delay in delivery due to any kind of reasons.
Refund of hard copy will not be provided after dispatch or print of the journal.
NN Publication will be responsible for raise a complain if there is any issue occurs in delivery, but still will not be responsible for providing the refund.
NN Publication will be responsible to resend the print copy only and only if the print copy is lost or print copy is damaged in delivery / or there is delay more than 6 months.
According to India Post the delivery should be completed with in 1-3 weeks after dispatch of articles.
Privacy Policy-
NN Publicationl uses the email ids of authors and editors and readers for sending editorial or publication notification only, we do not reveal or sell the email ids to any other website or company.
