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Journal articles on the topic 'Nano-satellites'

Author: Grafiati

Published: 4 June 2021

Last updated: 7 February 2022

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1

Лапханов, Эрик Александрович, та Александр Сергеевич Палий. "СОВРЕМЕННЫЕ ЗАДАЧИ СОЗДАНИЯ И УВОДА С ОРБИТЫ ГРУППИРОВОК КОСМИЧЕСКИХ АППАРАТОВ КЛАССА НАНО И ПИКО". Aerospace technic and technology, № 4 (14 жовтня 2018): 20–35. http://dx.doi.org/10.32620/aktt.2018.4.03.

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The purpose of the present paper is the analysis of current tasks concerning with creation and deorbiting of the formation flying groups consist of nano- and picosatellites and the consideration of the possibility of using permanent magnet devices for the deorbiting of these groups. During research was determined that it is most expedient to use small standardized spacecraft and use them during the development of distributed satellite systems. It can be both formations, and groups of satellites spaced a long distance. The analysis of the current possibilities for the removal of nano- and pico-

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2

Modenini, Dario, and Paolo Tortora. "Verification Approaches for Nano- and Micro-Satellites." Aerospace 7, no. 4 (2020): 40. http://dx.doi.org/10.3390/aerospace7040040.

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3

Nebylov, A. V., and A. E. Medina Padron. "Relative Motion Control of Nano-Satellites Constellation." IFAC-PapersOnLine 48, no. 9 (2015): 245–50. http://dx.doi.org/10.1016/j.ifacol.2015.08.091.

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4

Khandekar, Pravin, Kanishka Biswas, Dushyant Kothari, and H. Muthurajan. "Nano Mechanical Properties of Ceramic Polymer Composite Micro Thruster Developed Using 3D Printing Technology." Advanced Science Letters 24, no. 8 (2018): 5884–90. http://dx.doi.org/10.1166/asl.2018.12214.

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Nano and micro satellites, when revolving around the earth, may drift by very small angle from their orbit. But this small angle drift may result in large deviation from their original orbit over a long distance which these satellite covers over a period of time. For the course correction of these satellites, very small thrust is required in specific direction. Normal propulsion system cannot serve this purpose, because the thrust may be too large for these satellites. That’s where the role of micro thrusters becomes important. These are MEMS devices which can produce very small thrust and can

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5

OGAWA, Hiroto, Ryota INOUE, Tsuyoshi TOTANI, Masashi WAKITA, and Harunori NAGATA. "S192022 Thermal design of micro-satellites and nano-satellites on sun-synchronous orbits." Proceedings of Mechanical Engineering Congress, Japan 2011 (2011): _S192022–1—_S192022–5. http://dx.doi.org/10.1299/jsmemecj.2011._s192022-1.

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6

Cao, Shengzhu, Xuekang Chen, Gan Wu, et al. "Variable Emissivity Surfaces for Micro and Nano-satellites." Physics Procedia 18 (2011): 91–94. http://dx.doi.org/10.1016/j.phpro.2011.06.064.

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7

NAKASUKA, Shinichi. "Challenge to New Space Development Utilizing Nano-satellites." Proceedings of the Materials and processing conference 2010.18 (2010): A1—A5. http://dx.doi.org/10.1299/jsmemp.2010.18.a1.

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8

Yao, Yuan, Zhiguo Jiang, Haopeng Zhang, and Yu Zhou. "On-Board Ship Detection in Micro-Nano Satellite Based on Deep Learning and COTS Component." Remote Sensing 11, no. 7 (2019): 762. http://dx.doi.org/10.3390/rs11070762.

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Micro-nano satellites have provided a large amount of remote sensing images for many earth observation applications. However, the hysteresis of satellite-ground mutual communication of massive remote sensing images and the low efficiency of traditional information processing flow have become the bottlenecks for the further development of micro-nano satellites. To solve this problem, this paper proposes an on-board ship detection scheme based on deep learning and Commercial Off-The-Shelf (COTS) component, which can be used to achieve near real-time on-board processing by micro-nano satellite co

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9

Cao, Sheng Zhu, Xue Kang Chen, Gan Wu, Jian Ping Yang, and Rui Wang. "Micro Louvers for Micro and Nano-Satellites Thermal Control." Advanced Materials Research 317-319 (August 2011): 1658–61. http://dx.doi.org/10.4028/www.scientific.net/amr.317-319.1658.

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Micro and Nano-satellites with their low thermal capacitance are vulnerable to rapid temperature fluctuations. Therefore, thermal control becomes more important, but the limitations on mass and electrical power require new approaches. Possible solutions to actively vary the heat rejection of the satellite in response to variations in the thermal load and environmental condition are the use of variable emissivity devices, such as micro louvers, micro thermal switches, etc. Micro louvers with small volume, low weight, less power consumption and large emissivity variation, will be the more suitab

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10

Sabadosh, Lyubomyr, Serhii Larkov, Oleg Kravchenko, and Vladyslav Sereda. "Increasingly Safe, High-Energy Propulsion System for Nano-Satellites." Transactions on Aerospace Research 2018, no. 4 (2018): 38–44. http://dx.doi.org/10.2478/tar-2018-0028.

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Summary Numerous attempts have been undertaken to develop propulsion systems for nano-satellite-type spacecrafts to enable their maneuvering in orbits. One of the potentially viable chemical propellant propulsion systems is a hybrid system. The present paper studies propellant composition variants with the metal hydride as fuel that can be chosen for a nano-satellite hybrid propulsion system. It defines key requirements for chemical propellant nano-satellite propulsion systems, and specifies potential propellant pairs based on a compact metal hydride. The study describes basic technical charac

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11

SHIMIZU, Morio, and Hironori SAHARA. "205 Solar Thermal Propulsion System for Micro/Nano Satellites." Proceedings of Conference of Kyushu Branch 2001.54 (2001): 43–44. http://dx.doi.org/10.1299/jsmekyushu.2001.54.43.

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12

Ferreira, J. L., A. A. Martins, R. A. Miranda, M. C. F. Porto, and H. O. Coelho. "Hall plasma thruster development for micro and nano satellites." Journal of Physics: Conference Series 1365 (October 2019): 012026. http://dx.doi.org/10.1088/1742-6596/1365/1/012026.

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13

Sansone, Francesco, Alessandro Francesconi, Roberto Corvaja, et al. "LaserCube optical communication terminal for nano and micro satellites." Acta Astronautica 173 (August 2020): 310–19. http://dx.doi.org/10.1016/j.actaastro.2020.04.049.

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14

Tovar Soto, Jhonatan Paolo, Carlos Francisco Pareja Figueredo, Jonathan Steven Vargas Cañón, and Luis Carlos Gutiérrez Martínez. "A review of the current state of Pico and Nanosatellites: some applications in Latin America and other regions of the world." GRAINE. Boletín de Investigaciones. 2, no. 1 (2020): 13–30. http://dx.doi.org/10.52408/vol2iss1pp13-30.

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Small satellites have been a fundamental factor in the constant growth of space technologies from 60 years ago. Since the space war began during the Cold War, thousands of satellites have been put into low orbit to carry out radio frequency applications, analysis and sending satellite images of the earth, joint research tasks for space exploration on artificial satellites, as well as missions in other astronomical bodies. By 2019, more than 50 countries around the world have put into orbit at least 1 small satellite, which accounts for the persistent work to increase the applications of these

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15

Tovar Soto, Jhonatan Paolo, Carlos Francisco Pareja Figueredo, Jonathan Steven Vargas Cañón, and Luis Carlos Gutiérrez Martínez. "A review of the current state of Pico and Nanosatellites: some applications in Latin America and other regions of the world." GRAINE. Boletín de Investigaciones. 2, no. 1 (2020): 13–30. http://dx.doi.org/10.52408/gbdivol2iss1pp13-30.

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Small satellites have been a fundamental factor in the constant growth of space technologies from 60 years ago. Since the space war began during the Cold War, thousands of satellites have been put into low orbit to carry out radio frequency applications, analysis and sending satellite images of the earth, joint research tasks for space exploration on artificial satellites, as well as missions in other astronomical bodies. By 2019, more than 50 countries around the world have put into orbit at least 1 small satellite, which accounts for the persistent work to increase the applications of these

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16

Savu, G. "Micro, nano and pico satellites launched from the Romanian territory." Acta Astronautica 59, no. 8-11 (2006): 858–61. http://dx.doi.org/10.1016/j.actaastro.2005.07.004.

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17

RAJA, M., and O. PRAKASH. "Design of High Pointing Accuracy NPSAT-1 Satellite Attitude Systems of Armature Controlled DC Motor with utilization for PD Controller." INCAS BULLETIN 12, no. 1 (2020): 145–56. http://dx.doi.org/10.13111/2066-8201.2020.12.1.14.

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An Attitude control system plays the important role to maintain the satellite to desired attitude orientations. The intended application of NANO satellite in low earth orbits (LEO) helps find transient responses with and without controllers. LEO satellites typically orbit at an altitude ranging between160-2000 km. LEO satellites are widely used for remote sensing, navigation, and military surveillance applications. The Nano NPSAT-1 satellite attitude control systems (ACS) are described in this research work. The high pointing accuracy attitude estimation and feedback control systems are presen

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18

HATAMURA, Toru, Hirokazu MASUI, Mengu CHO, and Kazuo MAENO. "The Simulation about Adjustment Method of Shock Level of Nano Satellites." JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 63, no. 3 (2015): 117–19. http://dx.doi.org/10.2322/jjsass.63.117.

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19

Maeno, Masaki, and Saburo Matsunaga. "C2 Development of Distributed Ground Station Network system for Nano-Satellites." Proceedings of the Space Engineering Conference 2007.16 (2008): 61–65. http://dx.doi.org/10.1299/jsmesec.2007.16.61.

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20

SAKAMOTO, Yuji. "S192026 International Orbit Determination Network System for Micro and Nano Satellites." Proceedings of Mechanical Engineering Congress, Japan 2012 (2012): _S192026–1—_S192026–4. http://dx.doi.org/10.1299/jsmemecj.2012._s192026-1.

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21

AHEIEVA, Kateryna, Kazuhiro TOYODA, and Mengu CHO. "Vacuum Arc Thruster Development and Testing for Micro and Nano Satellites." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 14, ists30 (2016): Pb_91—Pb_97. http://dx.doi.org/10.2322/tastj.14.pb_91.

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22

Stacul, Adrián, Daniel Pastafiglia, Ariel Di Giovanni, et al. "A hardware system with ARM-based data processing for nano satellites." International Journal of Reconfigurable and Embedded Systems (IJRES) 9, no. 2 (2020): 102. http://dx.doi.org/10.11591/ijres.v9.i2.pp102-108.

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<span>The Institute of Scientiﬁc and Technical Research for Defense in Argentina (Instituto de Investigaciones Cientíﬁcas y Técnicas para la Defensa - CITEDEF) is developing a processing hardware module based on a ARM Cortex M4 processor from STMicroelectronics. The microcontroller (MCU) has the capacity to run at a maximum clock frequency of 180 MHz, integrates a Floating Point Unit (FPU). An 8MB SDRAM was included for dynamic data allocation. This hardware will host and process the algorithms to calculate and determine the nanosatellite’s attitude. The module is intended to be Cubesat

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23

Gill, E., P. Sundaramoorthy, J. Bouwmeester, B. Zandbergen, and R. Reinhard. "Formation flying within a constellation of nano-satellites: The QB50 mission." Acta Astronautica 82, no. 1 (2013): 110–17. http://dx.doi.org/10.1016/j.actaastro.2012.04.029.

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24

Burton, R., S. Rock, J. Springmann, and J. Cutler. "Dual attitude and parameter estimation of passively magnetically stabilized nano satellites." Acta Astronautica 94, no. 1 (2014): 145–58. http://dx.doi.org/10.1016/j.actaastro.2013.08.017.

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25

Lee, Jongkwang, and Taegyu Kim. "Micro space power system using MEMS fuel cell for nano-satellites." Acta Astronautica 101 (August 2014): 165–69. http://dx.doi.org/10.1016/j.actaastro.2014.04.010.

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26

Kuwahara, T., Y. Tomioka, K. Fukuda, et al. "Impacts of Space Plug-and-Play Technology on Micro- and Nano-satellites." IFAC Proceedings Volumes 46, no. 19 (2013): 289–94. http://dx.doi.org/10.3182/20130902-5-de-2040.00109.

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27

Nakasuka, Shinichi. "New Paradigm of Space Development and Utilization Created by Micro/nano-satellites." Journal of the Society of Mechanical Engineers 116, no. 1134 (2013): 319–22. http://dx.doi.org/10.1299/jsmemag.116.1134_319.

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28

Imai, Katsutoshi, Naoki Miyashita, Masafumi Iai, et al. "Examination of Bus System Components and Missions for 20kg Class Nano-Satellites." Proceedings of the Space Engineering Conference 2004.13 (2005): 49–54. http://dx.doi.org/10.1299/jsmesec.2004.13.49.

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29

Ortega, P., Gema López-Rodríguez, J. Ricart, et al. "A Miniaturized Two Axis Sun Sensor for Attitude Control of Nano-Satellites." IEEE Sensors Journal 10, no. 10 (2010): 1623–32. http://dx.doi.org/10.1109/jsen.2010.2047104.

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30

SAITO, Shin-nosuke, Tomonori ITOU, Shin SATORI, and Kazuhisa CHIBA. "523 TeleCommunication of Large-size Data Using Visble Light for Nano-Satellites." Proceedings of Conference of Hokkaido Branch 2014.53 (2014): 135–36. http://dx.doi.org/10.1299/jsmehokkaido.2014.53.135.

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31

Eunjeong Lee. "A micro HTS renewable energy/attitude control system for micro/nano satellites." IEEE Transactions on Appiled Superconductivity 13, no. 2 (2003): 2263–66. http://dx.doi.org/10.1109/tasc.2003.813061.

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32

Paek, S. W., S. Kim, L. Kronig, and O. de Weck. "Sun-synchronous repeat ground tracks and other useful orbits for future space missions." Aeronautical Journal 124, no. 1276 (2020): 917–39. http://dx.doi.org/10.1017/aer.2020.21.

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ABSTRACTThe development of oceanography and meteorology has greatly benefited from satellite-based data of Earth’s atmosphere and ocean. Traditional Earth observation missions have utilised Sun-synchronous orbits with repeat ground tracks due to their advantages in visible and infrared wavelengths. However, diversification of observation wavelengths and massive deployment of miniaturised satellites are both enabling and necessitating new kinds of space missions. This paper proposes several unconventional satellite orbits intended for use in, but not limited to, Earth observation. This ‘toolbox

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33

Zhou, Liang, Jian-jun Luo, Tiago Nogueira, and Klaus Schilling. "Orbit design and control method for satellite clusters and its applications to NetSat project." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, no. 8 (2017): 1559–70. http://dx.doi.org/10.1177/0954410017696109.

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In this paper, an optimal orbit design and control method for satellite clusters is presented and the method is applied to the four pico/nano-satellite system NetSat. Firstly, the relative motion based on relative eccentricity/inclination vectors is reviewed. Then, an optimal orbit design method for the cluster flight is developed, and the initial states of satellites in the cluster are derived using a graphical representation of the relative eccentricity/inclination vectors combined with a constrained nonlinear programming method. Next, a novel satellite cluster feedback control method is des

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34

Quiroga, Juan Jorge, Jorge Lassig, and Darío Mendieta. "Pehuensat-1." International Journal of Space Technology Management and Innovation 3, no. 2 (2013): 47–77. http://dx.doi.org/10.4018/ijstmi.2013070103.

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Nowadays, it is possible to achieve low cost and short production times space missions using satellites with a mass below 10 kg. These small satellites are described as nanosatellites. Current microelectronic technology makes it possible to develop nanosatellites for scientific experiments and relatively complex measurements (as well as for other applications), making it easy for universities and small research groups to have access to space science exploration and to exploit the new economic possibilities that emerge. This paper describes an experiment developed in Argentina at the Universida

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35

Grm, Aleksander, Tor‐Arne Grönland, and Tomaž Rodič. "Numerical analysis of a miniaturised cold gas thruster for micro‐ and nano‐satellites." Engineering Computations 28, no. 2 (2011): 184–95. http://dx.doi.org/10.1108/02644401111109222.

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36

Vieira, Juner, Marcelo Pereira Magalhães, Marcos Vinicio Thomas Heckler, João Cesar Moura Mota, and Antonio Sergio Sombra. "Development of an UHF 2 x 2 Microstrip Antenna Array for Nano-Satellites." Journal of Communication and Information Systems 31, no. 1 (2016): 137–45. http://dx.doi.org/10.14209/jcis.2016.13.

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37

NAKASUKA, Shinichi, Kei SENDA, Akihito WATANABE, Takashi YAJIMA, and Hironori SAHARA. "Simple and Small De-orbiting Package for Nano-Satellites Using an Inflatable Balloon." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN 7, ists26 (2009): Tf_31—Tf_36. http://dx.doi.org/10.2322/tstj.7.tf_31.

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38

TOTANI, Tsuyoshi, Ryota INOUE, Hiroto OGAWA, Tilok Kumar DAS, Masashi WAKITA, and Harunori NAGATA. "New Procedure for Thermal Design of Micro- and Nano-satellites Pointing to Earth." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 12, ists29 (2014): Pf_11—Pf_20. http://dx.doi.org/10.2322/tastj.12.pf_11.

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39

Kazokaitis, Gražvydas, Vytautas Jūrėnas, and Darius Eidukynas. "Research and analysis of spherical magnetic drive for attitude control on nano satellites." Vibroengineering PROCEDIA 15 (December 1, 2017): 50–55. http://dx.doi.org/10.21595/vp.2017.19431.

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40

ODA, Yasuhisa, Shinichi NAKASUKA, and Priya FERNANDO. "A Correction Method of Orbit Elements Using Amateur Radio Facilities for Nano-Satellites." SPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 7 (2008): 33–36. http://dx.doi.org/10.2322/stj.7.33.

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41

Cen, J. W., and J. L. Xu. "A new prototype of self-pressurizing fuel tank for micro and nano-satellites." Acta Astronautica 64, no. 4 (2009): 410–15. http://dx.doi.org/10.1016/j.actaastro.2008.09.012.

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42

Liu, Pengfei, Xiaoqian Chen, and Yong Zhao. "Safe deployment of cluster-flying nano-satellites using relative E/I vector separation." Advances in Space Research 64, no. 4 (2019): 964–81. http://dx.doi.org/10.1016/j.asr.2019.05.036.

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43

NAKAMURA, Yuya, Yasuhisa ODA, Mitsuhito KOMATSU, and Shinichi NAKASUKA. "3336 Low-Cost Ground Station Network To Improve Operation Efficiency for Micro/Nano-Satellites." Proceedings of the JSME annual meeting 2005.5 (2005): 399–400. http://dx.doi.org/10.1299/jsmemecjo.2005.5.0_399.

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44

Ohta, Kei, Shota Kawajiri, Kazuyoshi Miyasato, Masaya Koga, Yoichi Yatsu, and Saburo Matunaga. "E06 Proposal of an Automatic Operation System for Nano Satellites Using Multiple Ground Stations." Proceedings of the Space Engineering Conference 2014.23 (2014): _E06–1_—_E06–5_. http://dx.doi.org/10.1299/jsmesec.2014.23._e06-1_.

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45

Oh, Hyungjik, Do-hyun Kim, Ki-Yun Park, et al. "Development of On-board Computer Module for Formation Flying and Cluster Operation Nano-satellites." Journal of the Korean Society for Aeronautical & Space Sciences 47, no. 10 (2019): 728–37. http://dx.doi.org/10.5139/jksas.2019.47.10.728.

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46

SAKAMOTO, Yuji. "Orbit Determination Network System for Micro and Nano Satellites Using Low-Cost Ground Stations." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 12, ists29 (2014): Pf_21—Pf_26. http://dx.doi.org/10.2322/tastj.12.pf_21.

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47

Yamada, Kouhei, and Hosei Nagano. "Development of a heat storage panel for micro/nano-satellites and demonstration in orbit." Applied Thermal Engineering 91 (December 2015): 894–900. http://dx.doi.org/10.1016/j.applthermaleng.2015.08.073.

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48

YU, YAO, MIN GU, LILI ZHANG, TONG B. TANG, ZHAOSHENG LI, and TAO YU. "7Li NMR STUDY ON SURFACE IONIC DIFFUSION IN NANOCRYSTALLINE LiNbO3." Surface Review and Letters 14, no. 04 (2007): 583–86. http://dx.doi.org/10.1142/s0218625x07009888.

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By a wet chemical method we have prepared nano- LiNbO 3 with different crystallite sizes. Their 7 Li NMR spectra each show, on top of a broad band accompanied by two satellites, a sharp central peak whose strength decreases with growing grain size. On the other hand, for a given sample and as temperature rises, the separation between the two satellites gets wider, but the sharp peak gets narrower. From the satellite splitting we may estimate the molar ratio [ Li ]/[ Nb ] inside the nanocrystals, and this ratio is seen to be nearer to unity in a sample of smaller grain size. The sharp peak, ind

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49

Suehiro, Tomoya. "Satellite Design Methodology To Suppress Time-varying Residual Magnet Effects on Attitude For Nano-Satellites." IFAC Proceedings Volumes 43, no. 15 (2010): 241–46. http://dx.doi.org/10.3182/20100906-5-jp-2022.00042.

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50

INOUE, Ryota, Hiroto OGAWA, Tsuyoshi TOTANI, Masashi WAKITA, and Harunori NAGATA. "S192011 Thermal Analyses and Thermal Design of Nano and Micro Satellites on Sun-synchronous Orbits." Proceedings of Mechanical Engineering Congress, Japan 2012 (2012): _S192011–1—_S192011–5. http://dx.doi.org/10.1299/jsmemecj.2012._s192011-1.

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