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Relevant bibliographies by topics / Large space deployable antennas

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Academic literature on the topic 'Large space deployable antennas'

Author: Grafiati

Published: 4 June 2021

Last updated: 13 February 2022

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Journal articles on the topic "Large space deployable antennas"

1

Henriksen, T. K., and C. Mangenot. "Large deployable antennas." CEAS Space Journal 5, no. 3-4 (November 23, 2013): 87–88. http://dx.doi.org/10.1007/s12567-013-0055-4.

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2

He, Xing Xing, Ying Liao, and Ya Jun Yang. "Research on the Natural Frequency Prediction Method for Ring Tension Truss Deployable Antenna." Applied Mechanics and Materials 105-107 (September 2011): 2200–2203. http://dx.doi.org/10.4028/www.scientific.net/amm.105-107.2200.

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It is nearly impossible to carry out prototype experiments of large deployable space antennas because of their large dimensions. To solve this problem, a performance prediction approach is proposed in this paper. The prototype’s working performance is predicted by the scale model of the large deployable antenna. Based on this method, the natural frequency of the ring tension truss deployable antenna working in space is studied. The effect of the structural parameter distortion is taken into consideration by similarity criteria, and a similarity experimental formula of structural natural frequency is obtained. Four finite element models are established to validate the correction of the prediction method. The simulation results show that it’s valid for the prediction method to analyze the prototype in space, and it can be applied to promote the design, and performance prediction of the large deployable antennas.

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Lokman, Abdul Halim, Ping Jack Soh, Saidatul Norlyana Azemi, Herwansyah Lago, Symon K. Podilchak, Suramate Chalermwisutkul, Mohd Faizal Jamlos, Azremi Abdullah Al-Hadi, Prayoot Akkaraekthalin, and Steven Gao. "A Review of Antennas for Picosatellite Applications." International Journal of Antennas and Propagation 2017 (2017): 1–17. http://dx.doi.org/10.1155/2017/4940656.

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Cube Satellite (CubeSat) technology is an attractive emerging alternative to conventional satellites in radio astronomy, earth observation, weather forecasting, space research, and communications. Its size, however, poses a more challenging restriction on the circuitry and components as they are expected to be closely spaced and very power efficient. One of the main components that will require careful design for CubeSats is their antennas, as they are needed to be lightweight, small in size, and compact or deployable for larger antennas. This paper presents a review of antennas suitable for picosatellite applications. An overview of the applications of picosatellites will first be explained, prior to a discussion on their antenna requirements. Material and antenna topologies which have been used will be subsequently discussed prior to the presentation of several deployable configurations. Finally, a perspective and future research work on CubeSat antennas will be discussed in the conclusion.

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4

Cherniavsky, A. G., V. I. Gulyayev, V. V. Gaidaichuk, and A. I. Fedoseev. "Large Deployable Space Antennas Based on Usage of Polygonal Pantograph." Journal of Aerospace Engineering 18, no. 3 (July 2005): 139–45. http://dx.doi.org/10.1061/(asce)0893-1321(2005)18:3(139).

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5

Fanning, P., and L. Hollaway. "The Deployment Analysis of a Large Space Antenna." International Journal of Space Structures 8, no. 3 (September 1993): 209–20. http://dx.doi.org/10.1177/026635119300800307.

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The volume constraints imposed by current launch modules and the desirability of large reflectors and communication booms for space applications has given rise to active research in the field of deployable systems. These systems are stowed in a compact package for launch before being deployed into their operating configurations in orbit. A new concept for a deployable antenna is presented. The deployment of one such 5.0 m antenna is investigated. The antenna is deployed by a number of mechanical joints. The energy stored in these joints is quantified and the deployment times and stresses at ‘latch-up’ are predicted.

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6

Zheng, Fei, Mei Chen, Hai Ming Hao, and Jiu Li Zhang. "Deploying Analyses of Large Deployable Space Antenna under Gravity Environment." Advanced Materials Research 479-481 (February 2012): 2493–98. http://dx.doi.org/10.4028/www.scientific.net/amr.479-481.2493.

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The gravity is a serious problem for the deploying experiments of a large deployable space antenna on the ground. With the increasing trend for much bigger size deployable structures, new ground experiment methods with expected effects or with low cost should be explored. On this special object, we propose several deploying schemes from theoretical design, to practical design and then to actual design on a new folded hoop-rib mesh antenna structure we proposed before. Through the fundamental processes from theoretical analyses to actual experiments, it shows that the fairly complex mechanism can be deployed successfully, which reveals that the new deploying antenna structure design is feasible and reasonable.

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Ponomarev, Viktor S., Alexander V. Gerasimov, and Sergey V. Ponomarev. "Thermomechanical analysis of large deployable space reflector antenna." MATEC Web of Conferences 23 (2015): 01059. http://dx.doi.org/10.1051/matecconf/20152301059.

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8

Harada, Satoshi, Satoru Ozawa, Akira Meguro, and Mitsunobu Watanabe. "A shape analysis of membrane and cable structures for large space deployable antennas." Proceedings of the Space Engineering Conference 2003.11 (2003): 49–52. http://dx.doi.org/10.1299/jsmesec.2003.11.49.

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9

Zheng, Fei, Jie He, and Pan Zhang. "Simulating evaluation of new space deployable antenna." Aircraft Engineering and Aerospace Technology 88, no. 6 (October 3, 2016): 835–45. http://dx.doi.org/10.1108/aeat-08-2014-0123.

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Purpose The purpose of this paper is to build a new deployable antenna with folded scissors ribs and to evaluate the reasonable characteristics of this new structure. Design/methodology/approach Based on the TerrStar-1 satellite, virtual design and shapes forming are considered in this paper with the structure design of the new antenna. Considering the relaxation units in net surface, form-finding evaluation is used to build mathematical model and operate the optimization algorithm so that the design of the new antenna with folded scissors ribs is achieved. Simulations are carried out to verify the antenna proposed. Findings It is found that the antenna with folded scissors ribs can be developed smoothly in the space. Practical implications The proposed the antenna with folded scissors ribs can be considered as a fall-back alternative for large antenna, with a diameter of over 10 m in the space, or is seen as another option for the system with a simple rigid structure. Originality/value Different from traditional antenna, it provides a valuable reference for the further research of large deployable antenna in space. The antenna in this paper is able to develop more than 30 m of diameter. Meanwhile, the surface density and the natural frequency and the root-mean-square error in surface are superior to those of the traditional antenna.

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10

Chen, Mei, Fei Zheng, and Yuan Yuan Zhang. "Virtual Surface Measurement of Large Deployable Space Antenna Structure." Advanced Materials Research 479-481 (February 2012): 2586–92. http://dx.doi.org/10.4028/www.scientific.net/amr.479-481.2586.

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Virtual surface measurement is necessary to assist the actual measurement of large deployable space antenna structure. To realize a virtual surface measurement on this kind of structures, we take several steps to get the virtual measurement images. A virtual 3D model of the antenna structure and virtual hung system are constructed; virtual measure rules, coded marks and uncoded marks are also built up. The pinhole camera model is used to simulate the actual photogrammetric measurement tools. Through examples with OpenCV tools, the virtual measurement method is verified to be reasonable. Then different resolution images of perspective projections of the virtual measurement in virtual camera positions and orientations are obtained. Proper selections of the camera resolution and proper positions and orientations of the camera are found through virtual measurement experiments. Such results can be used in an actual photogrammetric measurement. The virtual measurement method can be used to reduce the attempt times and to assist the actual measurement with available photogrammetric measurement tools.

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Dissertations / Theses on the topic "Large space deployable antennas"

1

Smith, William Travis. "A synthesis procedure for array feeds to improve radiation performance of large distorted reflector antennas." Diss., This resource online, 1990. http://scholar.lib.vt.edu/theses/available/etd-07102007-142513/.

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Books on the topic "Large space deployable antennas"

1

Rogers, Craig A. Large Deployable Antenna Program. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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2

Rogers, Craig A. Large deployable antenna program: Phase I: Technology assessment and mission architecture. Hampton, Va: Langley Research Center, 1991.

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3

Duan, Baoyan, Yiqun Zhang, and Jingli Du. Large Deployable Satellite Antennas. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-6033-0.

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4

Schenk, Axel. Modal identification of a deployable space truss. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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5

Imbriale, William A. Large Antennas of the Deep Space Network. New York: John Wiley & Sons, Ltd., 2005.

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6

Padula, Sharon L. Integrated structure electromagnetic optimization of large space antenna reflectors. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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Padula, S. L. Integrated structure electromagnetic optimization of large space antenna reflectors. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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8

Dyer, J. E. Development of a verification program for deployable truss advanced technology. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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9

Joshi, Suresh M. Application of LQG/LTR technique to robust controller synthesis for a large flexible space antenna. Hampton, Va: Langley Research Center, 1986.

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10

Hamer, Harold A. Effects of model errors on control of large flexible space antenna with comparisons of decoupled and linear quadratic regulator control procedures. Hampton, Va: Langley Research Center, 1986.

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Book chapters on the topic "Large space deployable antennas"

1

Lawton, Mike, Juan R. Reveles, Zhong You, Ashley Dove-Jay, Amjad Khan, and Vincent Fraux. "Cost Disruptive Reflector Surface for Large Deployable Antennas." In Proceedings of the 13th Reinventing Space Conference, 95–105. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-32817-1_10.

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2

Focardi, Paolo, Paula R. Brown, and Yahya Rahmat-Samii. "Deployable Mesh Reflector Antennas for Space Applications: RF Characterizations." In Space Antenna Handbook, 314–43. Chichester, UK: John Wiley & Sons, Ltd, 2012. http://dx.doi.org/10.1002/9781119945147.ch8.

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3

Ganga, Pier Luigi, Andrea Micheletti, Paolo Podio-Guidugli, Lucio Scolamiero, Gunnar Tibert, and Valfredo Zolesi. "Tensegrity Rings for Deployable Space Antennas: Concept, Design, Analysis, and Prototype Testing." In Variational Analysis and Aerospace Engineering, 269–304. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-45680-5_11.

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4

Guang, Chenhan, Zilu Chen, and Yang Yang. "A Configuration Synthesis Method of Deployable Mechanism Cells Used for Large Supporting Structures in Space." In Mechanisms and Machine Science, 152–60. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-15-0142-5_16.

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5

Zhang, S., Q. Zhang, and F. Guan. "Surface adjustment on thermal deformation of a large deployable space structure." In Space Structures 5, 1: 635–639. Thomas Telford Publishing, 2002. http://dx.doi.org/10.1680/ss5v1.31739.0068.

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6

"Deep Space Station 12: Echo." In Large Antennas of the Deep Space Network, 79–88. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2005. http://dx.doi.org/10.1002/0471728497.ch3.

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7

"Deep Space Station 13: Venus." In Large Antennas of the Deep Space Network, 89–96. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2005. http://dx.doi.org/10.1002/0471728497.ch4.

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8

"Deep Space Station 14: Mars." In Large Antennas of the Deep Space Network, 97–156. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2005. http://dx.doi.org/10.1002/0471728497.ch5.

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9

"Deep Space Station 11: Pioneer-The First Large Deep Space Network Cassegrain Antenna." In Large Antennas of the Deep Space Network, 71–77. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2005. http://dx.doi.org/10.1002/0471728497.ch2.

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10

"The Next-Generation Deep Space Network." In Large Antennas of the Deep Space Network, 283–93. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2005. http://dx.doi.org/10.1002/0471728497.ch10.

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Conference papers on the topic "Large space deployable antennas"

1

Zheng, Fei, Mei Chen, and Peng Li. "Modeling of a Large Deployable Space Antenna Structure." In Modelling, Identification and Control. Calgary,AB,Canada: ACTAPRESS, 2012. http://dx.doi.org/10.2316/p.2012.769-071.

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2

Tian, Qiang, Jiang Zhao, Cheng Liu, Chunyan Zhou, and Haiyan Hu. "Dynamics of Space Deployable Structures." In ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/detc2015-46159.

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The space industry is eager to have the advanced technology of large space structures composed of trusses, cables and meshes. These space structures will deploy on orbit for different space missions. The important scientific basis of the technology is the nonlinear dynamic modeling, analysis and control of those space structures during their deployment and service. In this study, many space deployable structures (such as satellites antenna and spinning solar sail) are described by using the absolute nodal coordinate formulation (ANCF), and the huge set of equations of motion are solve by high efficient parallel generalized-alpha method. Some numerical results are also validated by experiment results.

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3

Sato, Takanori, Shinji Matsumoto, Haruyuki Namba, Kenji Takagi, Hisashi Tadokoro, Hiroshi Yamakawa, Takao Oura, Kenji Nozaki, and Nobuyuki Kaya. "Self Deployable Mechanism for Large Disk Antenna Using Centrifugal Force." In Fifth International Conference on Space. Reston, VA: American Society of Civil Engineers, 1996. http://dx.doi.org/10.1061/40177(207)156.

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4

Im, Eastwood, Mark Thomson, Houfei Fang, James Pearson, James Moore, and John Lin. "Prospects of Large Deployable Reflector Antennas for A New Generation of Geostationary Doppler Weather Radar Satellites." In AIAA SPACE 2007 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-9917.

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5

Sardhara Dipan, Y., S. H. Upadhyay, and S. P. Harsha. "Vibration Analysis of Inflatable Parabolic Structure for Space Application." In ASME 2012 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/detc2012-70828.

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Large deployable antennas for space applications become essential in the fields of communications, radio astronomy and Department of Defence (DOD) space-based radar. Since the antenna should be installed in a cargo space of a rocket vehicle during the launch phase, an inflatable deployment concept is inevitable to overcome the size limitation. A newly developed class of space structures, called inflatable-deployable structures, has great potential for satisfying these stringent user requirements. Among the many antenna types available, the parabolic reflector antenna is the most common one mainly due to its high gain, which enable high data rate transmission at low power. Large parabolic reflectors and solar concentrators are of great interest for the applications of satellite. This paper presents the finite element modelling of the parabolic shaped reflector to know the static and dynamic behaviour under the various inflation pressures. Purpose of this study is to highlight the dynamic characteristics of parabolic structures used in space application. The challenge is to assure that inflatable parabolic surfaces have significantly high efficiency and accuracy to satisfy the system requirements. Even the smart material is used for the control of the geometry of the reflecting surfaces and the study is done for the optimal size and placement of actuators and sensors the control of the shape of the reflecting surfaces. So this study is required to understand the dynamic characteristics i.e. frequency and mode shapes of these structures so that we can find out the maximum deflection and deformed shape of the parabolic surfaces.

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6

Cherniavsky, A. G., V. I. Gulyayev, V. V. Gaidaichuk, and A. I. Fedoseev. "New Developments in Large Deployable Space Antennae at S.P.A. EGS." In Ninth Biennial Conference on Engineering, Construction, and Operations in Challenging Environments. Reston, VA: American Society of Civil Engineers, 2004. http://dx.doi.org/10.1061/40722(153)130.

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7

OHKUBO, KUNITO, TAKAHIKO NODA, OSAMI ISHIDA, KAZUO YAMAMOTO, KORYO MIURA, and TADASHI TAKANO. "Development for a precision large deployable antenna for the space VLBI." In 14th International Communication Satellite Systems Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2011.

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8

Zheng, Fei, and Mei Chen. "System design and simulation of a new space large deployable antenna." In 2014 International Radar Conference (Radar). IEEE, 2014. http://dx.doi.org/10.1109/radar.2014.7060305.

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9

Fei Zheng, Mei Chen, and Peng Li. "Structural-electromagnetic performance prediction of a new large deployable space antenna." In 2010 IEEE Aerospace Conference. IEEE, 2010. http://dx.doi.org/10.1109/aero.2010.5446959.

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10

Lu, Shaolin, Xiaozhi Qi, Hailin Huang, Ying Hu, and Bing Li. "Accuracy Adjustment Method of Cable Net Surface for Large Space Deployable Antenna*." In 2018 IEEE International Conference on Information and Automation (ICIA). IEEE, 2018. http://dx.doi.org/10.1109/icinfa.2018.8812602.

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