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Journal articles on the topic 'Satellite layout'

Author: Grafiati

Published: 5 June 2025

Last updated: 2 August 2025

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1

Gong, Chang Qing, Zhen Chun Jiang, Chao Hui Huang, Ping Wang, and Tong Wu. "Optimization Analysis of GDOP of PL-Aided Navigation and Positioning System." Applied Mechanics and Materials 239-240 (December 2012): 544–47. http://dx.doi.org/10.4028/www.scientific.net/amm.239-240.544.

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The precision of satellite positioning system depends largely on the numbers and geometric layout of the positioning satellite, the GDOP is one of the important parameters to measure the geometric layout of positioning satellites. From the perspective of GDOP, the relation between a different pseudo-satellite location and layout for the accuracy of the positioning system has been studied. For the positioning of the four pseudo-satellites, the simulation analysis of the relationship of the GDOP parameter changes with the pseudo-satellite longitude, latitude and location of the user. Studies hav

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2

Feng, Jun Hong, and Li Deng. "Research on Geometric Layout of Pseudo-Satellite in the Small Airport." Applied Mechanics and Materials 651-653 (September 2014): 495–98. http://dx.doi.org/10.4028/www.scientific.net/amm.651-653.495.

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Because complex terrain conditions, the small airport satellite navigation signal being blocked, while reducing the positioning accuracy of the approach and landing segment, but also increase the operating costs of the small airport. This paper through independent pseudo-satellite network, from PDOP (Position Dilution of Precision) and VDOP (Vertical Dilution of Precision) studied several layout of airport pseudo-satellites. Through simulation show that the geometric layout of the pseudo-satellite can improve positioning accuracy of approach and landing segment in the small airport and reduce

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3

Xu, Zhi-Zheng, Chong-Quan Zhong, and Hong-Fei Teng. "Assignment and layout integration optimization for simplified satellite re-entry module component layout." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 12 (2017): 4287–301. http://dx.doi.org/10.1177/0954410017704220.

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Previous studies of satellite module component (equipment) layout optimization usually initialized a component assignment in the initialization stage, which kept constant in following optimization process. The invariable component assignment will restrict the further improvement in layout optimization. To overcome this deficiency, an assignment and layout integration optimization method is presented for multi-module or supporting surface satellite module component layout design. The assignment and layout integration optimization model and the component reassignment model are built. The compone

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Cui, Feng-Zhe, Chong-Quan Zhong, Xiu-Kun Wang, and Hong-Fei Teng. "A collaborative design method for satellite module component assignment and layout optimization." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 15 (2019): 5471–91. http://dx.doi.org/10.1177/0954410019847864.

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The collaborative design of the multi-module satellite component (equipment) assignment and layout is the key aspect of the overall satellite design, and the two parts are closely related. In the past, satellite module component layout optimization usually adopted fixed component assignments, which remained constant in the layout optimization stage. If the components were improperly distributed in these modules, it would seriously affect the layout optimization. To overcome this disadvantage, a collaborative design method for the component assignment and layout design is presented for the mult

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5

Tao, Cheng, Lei Zhang, Yihong Wang, et al. "An Extended Configuration Design of High-Throughput Satellite." Journal of Physics: Conference Series 2396, no. 1 (2022): 012049. http://dx.doi.org/10.1088/1742-6596/2396/1/012049.

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Abstract The high-throughput satellite (HTS) adopts multi-spot beam technology, which enables the satellite design process to be featured by a large number of antenna horns, large-scale arrays, heavy support structures, and complex interfaces with the transponder. To solve the layout problem of complex payloads of high-throughput satellites, this paper proposes a configuration design scheme for the satellite expansion module. With the configuration design optimization of the high-throughput satellite payload module of the DFH-4E platform serving as an example, the mechanical analysis software

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6

Zhang, Le, and Mingbo Bi. "Indoor Positioning Technology Based on Pseudo Satellite." Journal of Engineering Research and Reports 26, no. 9 (2024): 30–38. http://dx.doi.org/10.9734/jerr/2024/v26i91261.

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With the increasing demand for indoor positioning, traditional GPS positioning technology can no longer meet people's needs, and pseudo satellite indoor positioning technology has become a new method to solve indoor positioning problems. Pseudo satellite indoor positioning technology can improve positioning accuracy through the collaborative positioning of multiple signal sources and meet the positioning needs of different scenarios. Pseudo satellite indoor positioning technology can be applied to the field of smart home to achieve a more intelligent home environment and improve the quality of

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7

Zhang, Pengfei. "Research on satellite selection algorithm in ship positioning based on both geometry and geometric dilution of precision contribution." International Journal of Advanced Robotic Systems 16, no. 1 (2019): 172988141983024. http://dx.doi.org/10.1177/1729881419830246.

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With the networking of four Global Navigation Satellite Systems, the combination of multi-constellation applications has become an inevitable trend, and there will be more and more visible satellites that can be participated in ship positioning. However, the computational complexity increases sharply, which greatly improves the load capacity of the receiver’s data processor and reduces the output frequency of the positioning result. To achieve the balance between positioning accuracy and computational complexity, a new fast satellite selection algorithm based on both of geometry and geometric

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8

UTAMA, Satriya, Deddy El AMIN, M. Arif SAIFUDIN, et al. "Magnetic Shielding Implementation in the Small Satellite Reaction Wheel." INCAS BULLETIN 16, no. 1 (2024): 107–16. http://dx.doi.org/10.13111/2066-8201.2024.16.1.11.

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Low Earth orbit satellites face challenges from Earth's magnetic field, causing attitude disturbances. Attaining a magnetic-dipole-free satellite is crucial. Layout optimization and in-orbit dipole compensation are common methods, but layout optimization can be impractical. In contrast, in-orbit dipole compensation struggles with rapidly changing magnetic dipoles like those from reaction wheel motors. This research proposes an alternative solution using Mu-metal, known for shielding against magnetic exposure. This shield can be applied to trap the magnetic field generated by the motors. Ground

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9

Ahn, Byeongseon, and Ho-Yon Hwang. "Design Criteria and Accommodating Capacity Analysis of Vertiports for Urban Air Mobility and Its Application at Gimpo Airport in Korea." Applied Sciences 12, no. 12 (2022): 6077. http://dx.doi.org/10.3390/app12126077.

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This study establishes design criteria for touchdown and liftoff (TLOF) pads, final approach and takeoff (FATO), safety areas, gates, and taxiways, which are components necessary for the operation of vertiports for urban air mobility (UAM), and analyzed vertiport capacity compliant with the arrangement of the components in a limited space. We used new vertiport design regulations from the Federal Aviation Administration (FAA) and European Union Aviation Safety Agency (EASA) for the vertiport design criteria. Vertiport components were sized based on Hyundai Motor’s S-A1 aircraft, and the layout

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10

Koc, Wladyslaw. "Design of Reverse Curves Adapted to the Satellite Measurements." Advances in Civil Engineering 2016 (2016): 1–9. http://dx.doi.org/10.1155/2016/6503962.

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The paper presents a new method for designing railway route in the direction change area adapted to the Mobile Satellite Measurements technique. The method may be particularly useful in the situations when both tangents cannot be connected in an elementary way using a circular arc with transition curves. Thus, the only solution would be the application of two circular arcs of opposite curvature signs, that is, the use of an inverse curve. It has been assumed that the design of the geometrical layout will take place within an adequate local coordinate system. The solution of the design problem

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11

Chen, Xiaoqian, Xianqi Chen, Yufeng Xia, Weien Zhou, and Wen Yao. "An ILP-Assisted Two-Stage Layout Optimization Method for Satellite Payload Placement." Space: Science & Technology 2022 (September 28, 2022): 1–15. http://dx.doi.org/10.34133/2022/9765260.

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In the satellite overall design phase, it is a crucial step to perform satellite layout design to guarantee that the aggregation of electronic components can operate normally and stably in an appropriate temperature environment. In order to handle the satellite payload placement problem of the DongFangHong 4 (DFH-4) platform, the heat pipe-constrained component layout optimization (HCLO) problem is proposed with the HCLO model formulated. Through careful investigation, it can be divided into two optimization subproblems that can be solved subsequently. Based on the divide-and-conquer strategy,

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12

Zhang, Jiyao, Zhenqian Liu, Liwei Luo, Chunqiu Zhao, and Huayi Li. "Engineering-Oriented Layout Optimization and Trade-Off Design of a 12U CubeSat with In-Orbit Validation." Aerospace 12, no. 6 (2025): 506. https://doi.org/10.3390/aerospace12060506.

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The extensive application of CubeSats in fields such as communication, remote sensing, and scientific exploration highlights their significant engineering value. With the growth of CubeSat dimensions towards 12U and beyond, their potential for engineering applications has further expanded. However, strict size constraints significantly limit the layout design space, causing difficulties in satellite system design through multiple iterations. To address these practical issues, this paper proposes an engineering-oriented layout optimization and trade-off design approach tailored specifically for

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13

Wang, Jiangyong, Fa Jing, Yongquan Xia, and Chunsheng Xu. "Study on Model-Based System Engineering in Satellite Layout." MATEC Web of Conferences 316 (2020): 04001. http://dx.doi.org/10.1051/matecconf/202031604001.

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For satellite layout, it is necessary to collate manually in order to obtain accurate product technical requirements information. It is difficult to track the technical status information. It is proposed that the application of model-based system engineering (MBSE) in the cooperative development of multi-disciplinary and multisectoral satellite layout was an effective way to solve these problems. Based on the four typical processes of layout design, this paper studied the requirements to occupancy design, electromechanical joint design, integration of Attitude and Orbit Control System (AOCS) e

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14

Gamot, Juliette, Mathieu Balesdent, Romain Wuilbercq, Arnault Tremolet, and Nouredine Melab. "Two-Level Approach for Simultaneous Component Assignment and Layout Optimization with Applications to Spacecraft Optimal Layout." Applied Sciences 14, no. 18 (2024): 8120. http://dx.doi.org/10.3390/app14188120.

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Optimal layout problems consist in positioning a given number of components in order to minimize an objective function while satisfying geometrical or functional constraints. Such kinds of problems appear in the design process of aerospace systems such as satellite or spacecraft design. These problems are NP-hard, highly constrained and dimensional. This paper describes a two-stage algorithm combining a genetic algorithm and a quasi-physical approach based on a virtual-force system in order to solve multi-container optimal layout problems such as satellite modules. In the proposed approach, a

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15

Yeom, Seung-Yong, Hong-Rae Kim, and Young-Keun Chang. "3D Optimal Layout Design of Satellite Equipment." Journal of the Korean Society for Aeronautical & Space Sciences 43, no. 10 (2015): 875–87. http://dx.doi.org/10.5139/jksas.2015.43.10.875.

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16

Sun, Zhi-Guo, and Hong-Fei Teng. "Optimal layout design of a satellite module." Engineering Optimization 35, no. 5 (2003): 513–29. http://dx.doi.org/10.1080/03052150310001602335.

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17

Yishou, Wang, and Teng Hongfei. "Knowledge Fusion Design Method: Satellite Module Layout." Chinese Journal of Aeronautics 22, no. 1 (2009): 32–42. http://dx.doi.org/10.1016/s1000-9361(08)60066-7.

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18

Boissonnat, Jean-Daniel, Eelco de Lange, and Monique Teillaud. "Slicing Minkowski sums for satellite antenna layout." Computer-Aided Design 30, no. 4 (1998): 255–65. http://dx.doi.org/10.1016/s0010-4485(97)00074-2.

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19

Qin, Zheng, Yan-gang Liang, and Jian-ping Zhou. "An optimization tool for satellite equipment layout." Advances in Space Research 61, no. 1 (2018): 223–34. http://dx.doi.org/10.1016/j.asr.2017.10.030.

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20

Su, Jian Jiang, Chao Che, Qiang Zhang, and Xiao Peng Wei. "Satellite Module Layout Design Based on Adaptive Bee Evolutionary Genetic Algorithm." Applied Mechanics and Materials 538 (April 2014): 193–97. http://dx.doi.org/10.4028/www.scientific.net/amm.538.193.

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The main problems for Genetic Algorithm (GA) to deal with the complex layout design of satellite module lie in easily trapping into local optimality and large amount of consuming time. To solve these problems, the Bee Evolutionary Genetic Algorithm (BEGA) and the adaptive genetic algorithm (AGA) are introduced. The crossover operation of BEGA algorithm effectively reinforces the information exploitation of the genetic algorithm, and introducing random individuals in BEGA enhance the exploration capability and avoid the premature convergence of BEGA. These two features enable to accelerate the

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21

Huo, J.-Z., H.-F. Teng, W. Sun, and J. Chen. "Human-computer co-operative co-evolutionary method and its application to a satellite module layout design problem." Aeronautical Journal 114, no. 1154 (2010): 209–23. http://dx.doi.org/10.1017/s0001924000003663.

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Abstract The layout design of a satellite module is a complex mechanical layout problem. Its main difficulties lie in combinatorial explosion of computational complexity, engineering complexity, and applicability in engineering practice. Inspired by the human-computer cooperation ideas, a human–computer co-operative co-evolutionary method for optimising layout design of a satellite module is developed. This method constructs the diversity reference set by using the diversity intelligence solutions (DIs) that are created by using the combinatorial operators of differential evolution (DE) and th

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22

Zhong, Chong-Quan, Zhi-Zheng Xu, and Hong-Fei Teng. "Multi-module satellite component assignment and layout optimization." Applied Soft Computing 75 (February 2019): 148–61. http://dx.doi.org/10.1016/j.asoc.2018.11.021.

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23

Xiao, Zhiqi, Hao Jiang, Zhigang Deng, Ran Li, Wenwei Han, and Zhaoqi Wang. "Large Scale Farm Scene Modeling from Remote Sensing Imagery." ACM Transactions on Graphics 43, no. 6 (2024): 1–12. http://dx.doi.org/10.1145/3687918.

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In this paper we propose a scalable framework for large-scale farm scene modeling that utilizes remote sensing data, specifically satellite images. Our approach begins by accurately extracting and categorizing the distributions of various scene elements from satellite images into four distinct layers: fields, trees, roads, and grasslands. For each layer, we introduce a set of controllable Parametric Layout Models (PLMs). These models are capable of learning layout parameters from satellite images, enabling them to generate complex, large-scale farm scenes that closely reproduce reality across

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24

Hekmatfar, Masoud, M. R. M. Aliha, Mir Saman Pishvaee, and Tomasz Sadowski. "A Robust Flexible Optimization Model for 3D-Layout of Interior Equipment in a Multi-Floor Satellite." Mathematics 11, no. 24 (2023): 4932. http://dx.doi.org/10.3390/math11244932.

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Defanging equipment layout in multi-floor satellites consists of two primary tasks: (i) allocating the equipment to the satellite’s layers and (ii) placing the equipment in each layer individually. In reviewing the previous literature in this field, firstly, the issue of assigning equipment to layers is observed in a few articles, and regarding the layout, the non-overlapping constraint has always been a challenge, particularly for components that do not have a circular cross-section. In addition to presenting a heuristic method for allocating equipment to different layers of the satellite, th

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25

Wang, Xin, Guogang Wang, and Hongru Zheng. "Autonomous Phase Control Combining EKF and Adaptive Neural Network for Remote Sensing Satellites." International Journal of Aerospace Engineering 2022 (April 12, 2022): 1–16. http://dx.doi.org/10.1155/2022/7153667.

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In this paper, a novel, effective, and feasible autonomous phase control algorithm based on the extended Kalman filtering (EKF) and neural network is firstly developed for addressing the problems of configuration maintenance of remote sensing satellite constellation. A balanced moment arm optimization method is employed to design the installation structure layout of the chemical propulsion system in the satellite. On that basis, an autonomous orbit control strategy is presented for controlling the phase of satellites, and the EKF algorithm is utilized to determine the orbit used to calculate t

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26

Wang, Enyou, Jinxiu Zhang, Huayi Li, and Ming Liu. "Relative Position Model Predictive Control of Double Cube Test-Masses Drag-Free Satellite with Extended Sliding Mode Observer." Mathematical Problems in Engineering 2021 (January 22, 2021): 1–15. http://dx.doi.org/10.1155/2021/8887479.

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The drag-free satellites, being space-borne ultrahigh precise measurement platforms, have played irreplaceable roles in a great number of space science missions such as navigation, earth science, fundamental physics, and astrophysics. Most of these missions have to be performed based on the satellites placed with double cube test-masses, which makes the satellite layout and control strategy be more complex. This paper investigates the orbit keeping control problem of a class of low Earth orbit drag-free satellites with double cube test masses. A disturbance observer-based composite control met

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27

Khoddam, S., and M. A. Adrakani. "Passive control and layout optimization of Mesbah small satellite." Acta Astronautica 52, no. 9-12 (2003): 757–63. http://dx.doi.org/10.1016/s0094-5765(03)00051-1.

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28

Zhang, Bao, Hong-Fei Teng, and Yan-Jun Shi. "Layout optimization of satellite module using soft computing techniques." Applied Soft Computing 8, no. 1 (2008): 507–21. http://dx.doi.org/10.1016/j.asoc.2007.03.004.

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29

Xin, Jie, Dongxia Wang, and Kai Li. "An Integrity Monitoring Method for Navigation Satellites Based on Multi-Source Observation Links." Remote Sensing 16, no. 23 (2024): 4574. https://doi.org/10.3390/rs16234574.

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The BeiDou-3 navigation satellite system (BDS-3) has officially provided positioning, navigation, and timing (PNT) services to global users since 31 July 2020. With the application of inter-satellite link technology, global integrity monitoring becomes possible. Nevertheless, the content of integrity monitoring is still limited by the communication capacity of inter-satellite links and the layout of ground monitoring stations. Low earth orbit (LEO) satellites have advantages in information-carrying rate and kinematic velocity and can be used as satellite-based monitoring stations for navigatio

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30

Song, Xiaohui, Wei Wang, Xianing Xing, et al. "Study of Spacecraft Low Frequency Cable Installation Technology Oriented to CSB Bus." Journal of Physics: Conference Series 2209, no. 1 (2022): 012007. http://dx.doi.org/10.1088/1742-6596/2209/1/012007.

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Abstract In response to the needs of spacecraft cable three-dimensional crossover layout, research on cable installation methods based on CSB bus has been carried out. Aiming at the status of using CSB bus cable in the satellite communication cabin of DFH-4 platform for the first time, on the basis of detailed analysis of the performance of CSB bus, the laying and binding methods are analyzed and tested, and the cable installation method on the carbon fiber bracket is proposed. Technical solutions. It has been proved through practice that this method meets the actual needs of satellites, solve

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31

SHAO, Yu-jie, Yu Zhong-xi, Chun-lin DU, and Jing WANG. "Optimization Design of Thermal Test Waveguide Link for Communication Satellite." MATEC Web of Conferences 179 (2018): 03027. http://dx.doi.org/10.1051/matecconf/201817903027.

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Problems in structure of water load power meter and waveguide assemblies of the communication satellite transponder thermal test. This paper analyzes water load layout and reasons of signal attenuation, and then it proposes an optimization that put water load detached from satellite’s board. To ensure the reason of waveguide signal loss, this paper discusses the internal electromagnetic field distribution and currents on waveguide wall. the result of signal loss value showed that the new optimization can decrease signal attenuation value and shorten the process of crafts implementation.

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Awwad, Zeyad, Abdulaziz Alharbi, Abdulelah H. Habib, and Olivier L. de Weck. "Site Assessment and Layout Optimization for Rooftop Solar Energy Generation in Worldview-3 Imagery." Remote Sensing 15, no. 5 (2023): 1356. http://dx.doi.org/10.3390/rs15051356.

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With the growth of residential rooftop PV adoption in recent decades, the problem of effective layout design has become increasingly important in recent years. Although a number of automated methods have been introduced, these tend to rely on simplifying assumptions and heuristics to improve computational tractability. We demonstrate a fully automated layout design pipeline that attempts to solve a more general formulation with greater geometric flexibility that accounts for shading losses. Our approach generates rooftop areas from satellite imagery and uses MINLP optimization to select panel

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Liu, Qingzhi, Lei Huang, and Hua Yi. "Current status and suggestions of satellite borne single-phase fluid loops." Journal of Physics: Conference Series 2403, no. 1 (2022): 012035. http://dx.doi.org/10.1088/1742-6596/2403/1/012035.

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Abstract Enhancement of the load function and diversification put forward higher requirements for thermal control mode and the thermal rejection ability of the satellite. Limited to size, heat transfer efficiency, and mission characteristics of the satellite, thermal rejection ability has increasingly become one of the most important factors which restrict the mission of the satellite, and technical advantages and potential application of the single-phase fluid loops have become increasingly prominent. The single-phase fluid loop has been applied to China’s satellite field several times and ha

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34

Sparavigna, Amelia Carolina. "The orientation of the Kings Knot of Stirling Castle." PHILICA 2015 (December 27, 2015): 549. https://doi.org/10.5281/zenodo.3368834.

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In the satellite images of Google Earth we can easily see the King s Knot of the Stirling Castle, a knot garden made of earthworks with a geometric layout. Using SunCalc software, which is giving direction of sunrise and sunset on satellite maps, we can study the orientation of this Knot in relation to the apparent motion of the sun.

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Benxian Yue, Yishou Wang, Yanjun Shi, and Hongfei Teng. "Satellite Payloads Configuration and Layout Design Using Co-evolutionary Algorithm." International Journal of Advancements in Computing Technology 3, no. 11 (2011): 223–30. http://dx.doi.org/10.4156/ijact.vol3.issue11.28.

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36

Zheng, Qin, and Liang YanGang. "Layout Optimization of Satellite Cabin Considering Space Debris Impact Risk." Journal of Spacecraft and Rockets 54, no. 5 (2017): 1178–82. http://dx.doi.org/10.2514/1.a33719.

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Wang, Yi‐Shou, Hong‐Fei Teng, and Yan‐Jun Shi. "Cooperative co‐evolutionary scatter search for satellite module layout design." Engineering Computations 26, no. 7 (2009): 761–85. http://dx.doi.org/10.1108/02644400910985161.

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Gao, Yong-xin, Yi-min Ge, Ling-xi Ma, Yong-qiang Hu, and Yin-xin Chen. "Optimization Design of Configuration and Layout for Queqiao Relay Satellite." Advances in Astronautics Science and Technology 2, no. 1-2 (2019): 33–38. http://dx.doi.org/10.1007/s42423-019-00034-0.

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Harari, Mariaflavia. "Cities in Bad Shape: Urban Geometry in India." American Economic Review 110, no. 8 (2020): 2377–421. http://dx.doi.org/10.1257/aer.20171673.

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The spatial layout of cities is an important feature of urban form, highlighted by urban planners but overlooked by economists. This paper investigates the causal economic implications of city shape in India. I measure cities’ geometric properties over time using satellite imagery and historical maps. I develop an instrument for urban shape based on geographic obstacles encountered by expanding cities. Compact city shape is associated with faster population growth and households display positive willingness to pay for more compact layouts. Transit accessibility is an important channel. Land us

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40

Zhang, Yousheng. "A Method for micro-vibration test analysis of small satellites with laser loading." Journal of Physics: Conference Series 2764, no. 1 (2024): 012079. http://dx.doi.org/10.1088/1742-6596/2764/1/012079.

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Abstract Based on the parameters of the structure configuration and equipment layout of a small laser satellite in the design stage, the in-orbit micro-vibration simulation analysis of the satellite is carried out by finite element method, which mainly includes [1-2]: 1) modal analysis obtaining the main vibration frequency and modal shape of the satellite in orbit; 2) micro-vibration analysis of the satellite in orbit with the micro-vibration disturbance of the moment gyroscope as the excitation condition. Through the in-orbit micro-vibration simulation analysis of the satellite, we can obtai

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Wang, Gang, Fei Yang, Honghao Yue, and Shengyuan Jiang. "Optimal layout method of distributed locking device of satellite based on plant root growth theory." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 8 (2018): 2802–18. http://dx.doi.org/10.1177/0954410018786615.

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The method of determining the optimal direction of satellite locking point is extended from the mechanical stability principle of plant roots growth under external loads. The method of topological optimization of the number and location of satellite locking units was proposed based on the adventitious root growth pattern of monocotyledons. Inspired by the fibrous root growth rhythm, the method for topological optimization of the effective contact interface shape of the satellite locking units is presented. A satellite finite element model and three-dimensional spring support model are establis

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Cui, Feng-Zhe, Zhi-Zheng Xu, Xiu-Kun Wang, Chong-Quan Zhong, and Hong-Fei Teng. "A dual-system cooperative co-evolutionary algorithm for satellite equipment layout optimization." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, no. 13 (2017): 2432–57. http://dx.doi.org/10.1177/0954410017715280.

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This paper develops a new dual-system cooperative co-evolutionary algorithm for multi-modules (or multi-bearing plate) satellite equipment layout optimization problem, based upon the Potter’s cooperative co-evolutionary framework. Firstly, a new dual-system framework based on the Potter’s cooperative co-evolutionary is constructed and then, corresponding system decomposition rule, matrix analysis method and coordination mechanism are presented. Finally, the way of matching algorithms (e.g. evolutionary algorithms and swarm intelligence algorithms) with systems A and B in the dual system is pre

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A, Mohamed Shuaib. "Comprehensive Analysis of Satellite Deployment Dynamics using MATLAB." International Journal on Aerospace and Defence Research 1, no. 1 (2024): 29–36. http://dx.doi.org/10.69759/ijadr1105.

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A crucial section of area missions is satellite placement, which requires proper management and analysis to guarantee undertaking fulfilment. This paper presents a comprehensive framework for evaluation and simulation of satellite deployment dynamics based on MATLAB. The proposed framework combines visualization processes, dynamics of satellite deployment, and numerical methods to accurately model satellite behaviour all through deployment ranges. The simulation platform uses MATLAB's capability which includes thrust, aerodynamic drag, and gravitational forces to represent the complicated dyna

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Zhang, Bao. "Particle swarm optimization based on pyramid model for satellite module layout." Chinese Journal of Mechanical Engineering (English Edition) 18, no. 04 (2005): 530. http://dx.doi.org/10.3901/cjme.2005.04.530.

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M., Sanusi, Ibrahim Ndana M., Onyebuchi Gerald O., et al. "Satellite Operations Management, Nigeriasat-2 Experiences and Challenges." International Journal of Recent Research in Electrical and Electronics Engineering (IJRREEE) 10, no. 3 (2023): 22–27. https://doi.org/10.5281/zenodo.8388967.

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<strong>Abstract:</strong> Launching satellites and maintaining a mission while in orbit is a procedural and expensive activity. It is therefore imperative; satellite operations are designed to suit mission requirements so that operational activities are planned and managed properly. The earth station design and mission control planning are con-currently conducted with satellite payload and platform design and development. This strategy will ensure adequate testing of both satellite and ground facilities prior launching into the desired orbit. In this paper, Nigeriasat-2 ground segment managem

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Fan, Chen, Rong Yan, Cheng Tao, Yinglei Shan, and Cheng Li. "A structural layout and thermal control design of laser terminal on GEO satellite." Journal of Physics: Conference Series 2965, no. 1 (2025): 012013. https://doi.org/10.1088/1742-6596/2965/1/012013.

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Abstract Laser communication technology with characteristics of large communication capacity, high communication rate, low power consumption, and strong anti-jamming ability, shows great advantage on satellite communication. Meanwhile, the stability and uniformity indexes of the temperature of the laser antenna must be strictly controlled in order to ensure communication duration and quality. This paper proposes an expanded configuration layout and heat radiator + heat pipe type thermal control design scheme, takes a DFH-4E platform satellite laser terminal design scheme as an example, and car

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Shukla, Reedhi, Sampath Kumar Pabbisetty, Satish Jayanthi, and Kamini Janardhanan. "Evaluating the damage of collapsed bridges using remote sensing technologies: Case study: Baltimore’s Francis Scott Key Bridge." Eco Cities 5, no. 2 (2024): 2698. http://dx.doi.org/10.54517/ec.v5i2.2698.

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<p class="MsoNormal" style="line-height: 120%; layout-grid-mode: char; mso-layout-grid-align: none; margin: 12.0pt 0cm 6.0pt 147.4pt;"><span lang="EN-US" style="font-size: 10.0pt; line-height: 120%; mso-fareast-font-family: 'Times New Roman'; mso-font-kerning: 0pt; mso-fareast-language: JA; mso-no-proof: no;">Bridges are vital for linking communities and facilitating economic activity. However, in the face of disaster, like ship collisions pose a significant threat to bridge infrastructure, causing structural damage and potential safety hazards. Rapid and precise assessment of the

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Zheng, Qin, and Liang YanGang. "Multiobjective Methodology for Satellite Cabin Layout Optimization Considering Space Debris Impact Risk." Journal of Spacecraft and Rockets 55, no. 1 (2018): 232–35. http://dx.doi.org/10.2514/1.a33908.

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Hong-fei Teng, Yu Chen, Wei Zeng, Yan-jun Shi, and Qing-hua Hu. "A Dual-System Variable-Grain Cooperative Coevolutionary Algorithm: Satellite-Module Layout Design." IEEE Transactions on Evolutionary Computation 14, no. 3 (2010): 438–55. http://dx.doi.org/10.1109/tevc.2009.2033585.

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Shi, Yanjun, Bo Li, and Zihui Zhang. "Layout Design of Satellite Module Using a Modified Artificial Bee Colony Algorithm." Advanced Science Letters 4, no. 8 (2011): 3178–81. http://dx.doi.org/10.1166/asl.2011.1370.

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