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Power System Topology Proposal of a High-Altitude Pseudo-Satellite: Sizing Method, Power Budget Modeling and Efficient Power ControlSEDDJAR, A. , KERROUCHE, K. D. E. , KHORCHEF, N. |
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Author keywords
aerospace engineering, aerospace electronics, earth observing system, fuzzy control, power system control
References keywords
high(16), altitude(15), solar(12), design(11), pseudo(9), space(8), satellites(7), systems(6), power(6), endurance(6)
Blue keywords are present in both the references section and the paper title.
About this article
Date of Publication: 2022-02-28
Volume 22, Issue 1, Year 2022, On page(s): 47 - 56
ISSN: 1582-7445, e-ISSN: 1844-7600
Digital Object Identifier: 10.4316/AECE.2022.01006
Web of Science Accession Number: 000762769600001
SCOPUS ID: 85126811612
Abstract
In aerospace research, the High-Altitude Stratospheric Platform System (HAPS), is becoming an effective alternative solution to perform Earth observation missions, where several problems faced by aircraft systems can be solved. The most important advantages of HAPSs are their manufacturing and launch cost reduction compared to the satellites, with enough durability to provide services as satellites do. For a successful HAPS mission, it is imperative to assess the feasibility of their deployment in a given location, where, the energy generation and consumption are the main constraints. Therefore, the conception of an Electrical Power System (EPS) has been considered as a fundamental issue in HAPS development. In this paper, a proposed EPS topology, for HAPS dedicated to Earth observation missions, is presented with a proposed sizing method, power budget modeling, and a novel efficient power control based on fuzzy logic approach. |
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[1] J. Gonzalo, D. Lopez, D. DomÃnguez, A. GarcÃa, and A. Escapa, "On the capabilities and limitations of high altitude pseudo-satellites," Progress in Aerospace Sciences, vol. 98, pp. 37-56, 2018. [CrossRef] [Web of Science Times Cited 69] [SCOPUS Times Cited 112] [2] T. Fehr, M. Davidson, A. Ciccolella, and J. Lizarraga Cubillos, "High-altitude pseudo-satellites-an emerging tool in support of earth observation satellite development, calibration/validation and applications," in EGU General Assembly Conference Abstracts, 2018, p. 17497 [3] M. M. Fladeland, "Recent advances in high altitude pseudosatellites (HAPS) and potential roles in future earth observing systems," 2019 [4] R. Muller, J. J. Kiam, and F. Mothes, "Multiphysical simulation of a semi-autonomous solar powered high altitude pseudo-satellite," in 2018 IEEE Aerospace Conference, 2018, pp. 1-16 [5] F. Akram, H. Khan, T. Shams, and D. Mavris, "Design space optimisation of an unmanned aerial vehicle submerged inlet through the formulation of a data-fusion-based hybrid model," The Aeronautical Journal, pp. 1-18 [6] R. Dancila and R. Botez, "New flight trajectory optimisation method using genetic algorithms," The Aeronautical Journal, vol. 125, pp. 618-671, 2021. [CrossRef] [Web of Science Times Cited 13] [SCOPUS Times Cited 20] [7] A. Klockner, Behavior trees for mission management of high-altitude pseudo-satellites: Dr. Hut, 2016 [8] B. Kirsch and O. Montagnier, "Towards the advent of high-altitude pseudo-satellites (HAPS)," Disruptive Technology and Defence Innovation Ecosystems, vol. 5, pp. 181-201, 2019. [CrossRef] [9] T. Ma, Y. Liu, D. Yang, Z. Zhang, X. Wang, and S. Hao, "Research on the design of smart morphing long-endurance UAVs," The Aeronautical Journal, vol. 125, pp. 22-41, 2021. [CrossRef] [Web of Science Times Cited 4] [SCOPUS Times Cited 4] [10] A. Alsahlani, L. Johnston, and P. Atcliffe, "Design of a high altitude long endurance flying-wing solar-powered unmanned air vehicle," Progress in Flight Physics, vol. 9, pp. 3-24, 2017. [CrossRef] [11] W. H. Phillips, "Some design considerations for solar-powered aircraft," National Aeronautics and Space Administration, Hampton, VA (USA). Langley, 1980 [12] D. Park, Y. Lee, T. Cho, and C. Kim, "Design and performance evaluation of propeller for solar-powered high-altitude long-endurance unmanned aerial vehicle," International Journal of Aerospace Engineering, vol. 2018, 2018. [CrossRef] [Web of Science Times Cited 23] [SCOPUS Times Cited 35] [13] P. Oettershagen, A. Melzer, T. Mantel, K. Rudin, T. Stastny, B. Wawrzacz, T. Hinzmann, S. Leutenegger, K. Alexis, and R. Siegwart, "Design of small hand-launched solar-powered UAVs: From concept study to a multi-day world endurance record flight," Journal of Field Robotics, vol. 34, pp. 1352-1377, 2017. [CrossRef] [Web of Science Times Cited 62] [SCOPUS Times Cited 86] [14] B. Kranjec, S. Sladic, W. Giernacki, and N. Bulic, "PV system design and flight efficiency considerations for fixed-wing radio-controlled aircraft-A case study," Energies, vol. 11, p. 2648, 2018. [CrossRef] [Web of Science Times Cited 9] [SCOPUS Times Cited 8] [15] M. Brizon, "Solar energy generation model for high altitude long endurance platforms," ed, 2015 [16] T. Smith, M. Trancossi, D. Vucinic, C. Bingham, and P. Stewart, "Primary and albedo solar energy sources for high altitude persistent air vehicle operation," Energies, vol. 10, p. 573, 2017. [CrossRef] [Web of Science Times Cited 7] [SCOPUS Times Cited 7] [17] D. Liviu, C. J. Ileana, and G. T. Lucian, "Energy conversion systems for high altitude pseudo-satellites," International Multidisciplinary Scientific GeoConference: SGEM: Surveying Geology & mining Ecology Management, vol. 17, pp. 223-230, 2017 [18] J. Barbe, A. Pockett, V. Stoichkov, D. Hughes, H. K. H. Lee, M. Carnie, T. Watson, and W. C. Tsoi, "In situ investigation of perovskite solar cells' efficiency and stability in a mimic stratospheric environment for high-altitude pseudo-satellites," Journal of Materials Chemistry C, 2020. [CrossRef] [Web of Science Times Cited 20] [SCOPUS Times Cited 22] [19] J.-I. Corcau, L. Dinca, M. Culcer, and M. Gheorghe, "Modeling and Simulation of Hybrid Power Source for Pseudo-Satellites," in 2018 International Symposium on Power Electronics, Electrical Drives, Automation and Motion (SPEEDAM), 2018, pp. 1055-1060. [CrossRef] [SCOPUS Times Cited 2] [20] K. Shin, H. Hwang, and J. Ahn, "Mission analysis of solar UAV for high-altitude long-endurance flight," Journal of Aerospace Engineering, vol. 31, p. 04018010, 2018. [CrossRef] [Web of Science Times Cited 10] [SCOPUS Times Cited 13] [21] S. C. Arum, D. Grace, P. D. Mitchell, M. D. Zakaria, and N. Morozs, "Energy management of solar-powered aircraft-based high altitude platform for wireless communications," Electronics, vol. 9, p. 179, 2020. [CrossRef] [Web of Science Times Cited 24] [SCOPUS Times Cited 30] [22] W. J. Larson and J. R. Wertz, "Space mission analysis and design," Torrance, CA (United States); Microcosm, Inc. 1992 [23] J. R. Wertz, and W. J. Larson, Space Mission Analysis and Design, 3rd ed., pp. 316, El Segundo, California, Microcosm Press and Kluwer Academic, 1999 [24] G. Warwick, "Record-breaking Zephyr's battery holds eVTOL potential: Amprius cells helped power Zephyr stratospheric UAV; company's current focus is on the aerospace market and high-performance UAVs," Aviation Week & Space Technology, 2019 [25] A. Defence, "Space,"Zephyr, the High Altitude Pseudo-Satellite," 2017," ed, 2017 [26] W. J. Larson and J. R. Wertz, "Space mission analysis and design," Torrance, CA (United States); Microcosm, Inc.1992. [CrossRef] [27] A. C. Maycock, W. J. Randel, A. K. Steiner, A. Y. Karpechko, J. Christy, R. Saunders, D. W. Thompson, C. Z. Zou, A. Chrysanthou, and N. Luke Abraham, "Revisiting the mystery of recent stratospheric temperature trends," Geophysical research letters, vol. 45, pp. 9919-9933, 2018. [CrossRef] [Web of Science Times Cited 56] [SCOPUS Times Cited 61] [28] A. Belkaid, I. Colak, and K. Kayisli, "Implementation of a modified P&O-MPPT algorithm adapted for varying solar radiation conditions," Electrical Engineering, vol. 99, pp. 839-846, 2017. [CrossRef] [Web of Science Times Cited 48] [SCOPUS Times Cited 69] [29] K. A. Mohamed, M. Zakareya, K. H. Youssef, and H. A. Khater, "Improved perturb and observe maximum peak power tracking for solar satellite systems," in IOP Conference Series: Materials Science and Engineering, 2019, p. 012091. [CrossRef] [SCOPUS Times Cited 1] [30] H. Taha, R. Mostafa, U. Abouzayed, and F. Eltohamy, "Design and Implementation of PV MPPT Controller based on modified P&O algorithm using FPGA for satellite systems," in 2018 13th International Conference on Computer Engineering and Systems (ICCES), 2018, pp. 524-529. [CrossRef] [SCOPUS Times Cited 1] [31] N. Altin, "Interval type-2 fuzzy logic controller based maximum power point tracking in photovoltaic systems," Advances in Electrical and Computer Engineering, vol. 13, pp. 65-71, 2013. [CrossRef] [Full Text] [Web of Science Times Cited 28] [SCOPUS Times Cited 38] [32] D. Petreus, D. Moga, A. Rusu, T. Patarau, and M. Munteanu, "Photovoltaic system with smart tracking of the optimal working point," Advances in Electrical and Computer Engineering, vol. 10, pp. 40-47, 2010. [CrossRef] [Full Text] [Web of Science Times Cited 8] [SCOPUS Times Cited 10] [33] A. Al-Gizi, S. Al-Chlaihawi, M. Louzazni, and A. Craciunescu, "Genetically optimization of an asymmetrical fuzzy logic based photovoltaic maximum power point tracking controller," Advances in Electrical and Computer Engineering, vol. 17, pp. 69-76, 2017. [CrossRef] [Full Text] [Web of Science Times Cited 6] [SCOPUS Times Cited 10] [34] R. Rahim, "Comparative analysis of membership function on Mamdani fuzzy inference system for decision making," in Journal of Physics Conference Series, 2017, p. 012029. [CrossRef] [Web of Science Times Cited 26] [SCOPUS Times Cited 75] [35] ESA, "Space engineering," in Electrical and electronic, ed. 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