• Title/Summary/Keyword: Solar Powered

Search Result 161, Processing Time 0.02 seconds

Modeling of Solar-Powered Hydrogen Production System using PSCAD/EMTDC (PSCAD/EMTDC를 이용한 수소제조용 태양광 발전 시스템의 모델링)

  • Lee Dong-Han;Park Minwon;Yu In-Keun
    • The Transactions of the Korean Institute of Electrical Engineers B
    • /
    • v.55 no.2
    • /
    • pp.116-121
    • /
    • 2006
  • This paper presents an effective modeling and simulation scheme of solar-powered hydrogen production system (PV-SPE: Photovoltaic Solid Polymer Electrolyte). Existing Hydrogen production technologies can produce vast amounts of hydrogen from hydrocarbons but emit large amounts of carbon dioxide (CO2) into the atmosphere. Advanced hydrogen production methods need development. Renewable technologies such as solar and wind need further development for hydrogen production to be more cost-competitive from other resources. In this paper, authors have focused on a renewable technology to move one step further toward commercial readiness of solar-powered hydrogen production system. Software (PSCAD/EMTDC) based model of PV-SPE system is studied for an effective simulation of hydrogen production system. Using the simulation results, an actual PV-SPE system is implemented to verify the simulation results by comparing them with actual values obtained from the data acquisition system.

A Study on 3.0m Low-Altitude Long-Endurance Solar Powered UAV System (3.0m급 저고도 장기체공 태양광 무인기 시스템 연구)

  • Jaebaek Jeong;Taerim Kim;Doyoung Kim;Seokmin Moon;Jae-Sung Bae;Sanghyuk Park
    • Journal of Aerospace System Engineering
    • /
    • v.17 no.4
    • /
    • pp.10-17
    • /
    • 2023
  • This paper describes the research and development of a 3.0 m Solar-Powered UAV system for mission flight that is based on the 4.2 m Solar-powered UAV. Both the Solar-Powered UAVs were lightened in weight by applying a composite fuselage and solar charging system. Also, a deep stall landing application and airbag module were installed for usability in mission performance. The flight performance of the Solar-Powered UAV system was verified through flight test. In particular, the 3.0 m Solar-Powered UAV performed continuous flight along the coastline of Jeju Island for 147 km in 3 hours and 50 minutes, and its performance as a mission flight was also confirmed.

Fuzzy Logic based Admission Control for On-grid Energy Saving in Hybrid Energy Powered Cellular Networks

  • Wang, Heng;Tang, Chaowei;Zhao, Zhenzhen;Tang, Hui
    • KSII Transactions on Internet and Information Systems (TIIS)
    • /
    • v.10 no.10
    • /
    • pp.4724-4747
    • /
    • 2016
  • To efficiently reduce on-grid energy consumption, the admission control algorithm in the hybrid energy powered cellular network (HybE-Net) with base stations (BSs) powered by on-grid energy and solar energy is studied. In HybE-Net, the fluctuation of solar energy harvesting and energy consumption may result in the imbalance of solar energy utilization among BSs, i.e., some BSs may be surplus in solar energy, while others may maintain operation with on-grid energy supply. Obviously, it makes solar energy not completely useable, and on-grid energy cannot be reduced at capacity. Thus, how to control user admission to improve solar energy utilization and to reduce on-grid energy consumption is a great challenge. Motivated by this, we first model the energy flow behavior by using stochastic queue model, and dynamic energy characteristics are analyzed mathematically. Then, fuzzy logic based admission control algorithm is proposed, which comprehensively considers admission judgment parameters, e.g., transmission rate, bandwidth, energy state of BSs. Moreover, the index of solar energy utilization balancing is proposed to improve the balance of energy utilization among different BSs in the proposed algorithm. Finally, simulation results demonstrate that the proposed algorithm performs excellently in improving solar energy utilization and reducing on-grid energy consumption of the HybE-Net.

Conceptual Design for Small Solar Powered Uninhabited Aerial Vehicle (소형 태양광 무인항공기의 개념 설계)

  • Lee, Sang-Hyup;Park, Sang-Hyuk;Bae, Jae-Sung
    • Journal of the Korean Society for Aviation and Aeronautics
    • /
    • v.19 no.2
    • /
    • pp.1-9
    • /
    • 2011
  • Several studies on the development for solar powered uninhabited aerial vehicles(UAVs) are under way as the use of the renewable energy becomes more and more important these days. This paper is for the conceptual design by a discrete and iterative method. An initial design point with 1.5 meter wing span is determined in the global design, which deploys the mass and energy balances among each component of UAV including solar cells and airframe. Then, the iteration for subsystems is carried out with the help of Vortex Lattice Method(VLM) to optimize the aircraft configuration and the solar power system. It is demonstrated in simulations that the optimized design increases the flight time from 62 to 120 minutes when the solar power system is installed. Also, the associated dynamic analysis reveals that the designed small aircraft has the acceptable stability and controllability.

Self-Powered Solar Tracker System without CPU (CPU 없는 자가 동력 태양광 트랙커 시스템)

  • Lee, Jae Jin;Choi, Woo Jin;Kim, Seok-Min;Park, Joon Young;Lee, Kyo-Beum
    • Journal of IKEEE
    • /
    • v.21 no.3
    • /
    • pp.211-218
    • /
    • 2017
  • This paper proposes the self-powered solar tracker system without CPU. Conventional solar tracker system occurs the problem of cost and durability because of using CPU. In addition, this system has effects from installation site and environment. The proposed solar tracker system without CPU is possible to achieve the high efficiency because it tracks the maximum of the light source. The validity of proposed solar tracking system is verified with experiment results.

Airframe Structure Development of Solar-powered HALE UAV EAV-3 (고고도 장기체공 태양광 무인기 EAV-3 기체구조 개발)

  • Shin, Jeong Woo;Park, Sang Wook;Lee, Sang Wook;Kim, Tae-Uk
    • Journal of the Korean Society for Aviation and Aeronautics
    • /
    • v.25 no.3
    • /
    • pp.35-43
    • /
    • 2017
  • Research for solar-powered high altitude long endurance(HALE) UAV was conducted by Korea Aerospace Research Institute(KARI), and the EAV-3 with 19.5m wing span was developed. For HALE flight, aircraft should be lightly designed. Especially, airframe structure that accounts for a large portion of the total weight of aircraft should be lightweight. In this paper, development process of airframe structure for solar-powered HALE UAV, EAV-3, is described briefly. Domestic developed T-800 grade CFRP(Carbon Fiber Reinforced Plastic) composite material with high modulus and strength was used to design main load carrying structures. Flightloads analysis that takes into account large structural deformation was carried out. Stress and flutter analyses for airframe structure sizing were conducted. Static strength test for main wing and aircraft ground vibration test were conducted successfully and structural integrity was secured.

A Study on Manufacturing Methods of Cocuring Composite Wings of Solar-Powered UAV (복합재 태양광 무인기 날개 일체성형 제작기법 연구)

  • Yang, Yongman;Kwon, Jeongsik;Kim, Jinsung;Lee, Sooyong
    • Journal of Aerospace System Engineering
    • /
    • v.10 no.1
    • /
    • pp.43-50
    • /
    • 2016
  • In order to suggest the optimal manufacturing technology of composite wings of solar-powered unmanned aerial vehicles, this study compared forming technologies to reduce wing weight for long-endurance flight and to improve the manufacturing process for cost-saving and mass production. It compared the manufacturing time and weight of various composite wing molding technologies, including cocuring, secondary bonding, and manufacturing by balsa. As a result, wing weight was reduced through cocuring methods such as band type composite fiber/tape lamination technology, which enabled prolonged flight duration. In addition, the reduced manufacturing time led to a lower cost, which is a good example of weight lightening for not only small solar-powered UAVs, but also composite aircraft.

Power Management Circuit for Self-Powered Systems Using Vibration and Solar Energy (진동 및 빛 에너지를 이용한 자가발전 시스템용 전력관리 회로)

  • Seo, Wan-Suck;Kim, Min-Kyu;Yu, So-Hyeon;Yoon, Eun-Jung;Park, Jun-Ho;Yu, Chong-Gun
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
    • /
    • 2011.10a
    • /
    • pp.419-422
    • /
    • 2011
  • In this paper a dual-input self-powered power management system is proposed for low-power applications. The system is powered by merging the energy from a PZT vibration element and a solar cell. The proposed system consists of a charge pump for increasing the output voltage of a solar cell, a rectifier for DC conversion of the PZT output and a power management circuit for merging and managing the harvested energy. The performance of the design circuit has been verified through extensive simulation using a 0.18um CMOS technology. The chip area is $295um{\times}275um$.

  • PDF

Sensing and Compression Rate Selection with Energy-Allocation in Solar-Powered Wireless Sensor Networks

  • Yoon, Ikjune
    • Journal of the Korea Society of Computer and Information
    • /
    • v.22 no.5
    • /
    • pp.81-88
    • /
    • 2017
  • Solar-powered wireless sensor nodes can use extra energy to obtain additional data to increase the precision. However, if the amount of data sensed is increased indiscriminately, the overhead of relay nodes may increase, and their energy may be exhausted. In this paper, we introduce a sensing and compression rate selection scheme to increase the amount of data obtained while preventing energy exhaustion. In this scheme, the neighbor nodes of the sink node determine the limit of data to be transmitted according to the allocated energy and their descendant nodes, and the other nodes select a compression algorithm appropriate to the allocated energy and the limitation of data to be transmitted. A simulation result verifies that the proposed scheme gathers more data with a lower number of blackout nodes than other schemes. We also found that it adapts better to changes in node density and the amount of energy harvested.

Architecture of the Solar-powered Sensor System for Distributed-storage Wireless Sensor Network (분산 저장형 센서 네트워크를 위한 태양 에너지 기반 센서 시스템의 구조)

  • Noh, Dong-Kun;Yoon, Ik-June
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
    • /
    • 2011.10a
    • /
    • pp.843-845
    • /
    • 2011
  • Due to the short lifetime of the battery-based sensor network, study on the environmental energy-harvesting sensor network is being performed widely. In this paper, we analyze the system-level requirements on the sensor node which is needed for the efficient solar-powered wireless sensor network for the target application. In addition, we explain how the HW/SW components of our real solar-powered sensor node can satisfy the requirements mentioned above.

  • PDF