Altitude control performance of a natural energy driven stratospheric aerostat

被引：7
|
作者：
Wu, Yao [1 ]
Wang, Chao [1 ]
Wang, Lei [1 ]
Ma, Rong [1 ]
Lu, Xiaochen [1 ]
Yao, Wei [1 ]
机构：
[1] China Acad Space Technol, Qian Xuesen Lab Space Technol, Beijing 100094, Peoples R China
来源：
ADVANCES IN SPACE RESEARCH | 2015年 / 56卷 / 11期
关键词：
Stratospheric aerostat; Thermo-mechanical model; Ascent process; Altitude control; THERMAL-BEHAVIOR; SIMULATION; OPTIONS; MODEL;
D O I：
10.1016/j.asr.2015.10.017
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The superheating induced overpressure is one of the key obstacles for long-endurance station-keeping of stratospheric aerostats. A novel stratospheric aerostat by utilizing the natural energy is presented and discussed in this paper. A thermo-mechanical dynamic model is established to analyze the altitude control performance of this novel aerostat. The simulation results show that the novel stratospheric aerostat can ascend to a high altitude about 25.8 km due to the combined heating effects of the solar radiation, the Earth albedo and the infrared radiation from the Earth's surface and keeps at an altitude about 22 km by the infrared radiation from the Earth's surface. In addition, the aerostat can be controlled within the desired altitude range by the simple open/close valve control strategy. (C) 2015 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：2508 / 2514
页数：7
相关论文
共 50 条
  • [31] SMARTS Modeling of Solar Spectra at Stratospheric Altitude and Influence on Performance of Selected III-V Solar Cells
    Limpinsel, Moritz
    Kuo, Dawei
    Vijh, Aarohi
    2018 IEEE 7TH WORLD CONFERENCE ON PHOTOVOLTAIC ENERGY CONVERSION (WCPEC) (A JOINT CONFERENCE OF 45TH IEEE PVSC, 28TH PVSEC & 34TH EU PVSEC), 2018, : 3367 - 3373
  • [32] The Use of Normative Energy Calculation for Natural Ventilation Performance-Driven Urban Block Morphology Generation
    Li, Wenjing
    Xu, Xinhui
    Makvandi, Mehdi
    Sun, Zhuoyang
    Yuan, Philip F.
    PHYGITAL INTELLIGENCE, CDRF 2023, 2024, : 315 - 328
  • [33] Composite control system of hybrid-driven mid-altitude airship
    Chen, L.
    Dong, Q.
    Zhang, G.
    Duan, D.
    AERONAUTICAL JOURNAL, 2018, 122 (1248): : 173 - 204
  • [34] Composite control system of hybrid-driven mid-altitude airship
    1600, Cambridge University Press (122):
  • [35] P promotion on the performance of Pd-based catalyst for emission control of natural gas driven vehicles
    Chen, Jianjun
    Hu, Wei
    Huang, Fujin
    Wu, Yang
    Yuan, Shandong
    Zhong, Lin
    Chen, Yaoqiang
    JOURNAL OF THE TAIWAN INSTITUTE OF CHEMICAL ENGINEERS, 2018, 91 : 323 - 331
  • [36] Static Analysis Driven Performance and Energy Testing
    Banerjee, Abhijeet
    22ND ACM SIGSOFT INTERNATIONAL SYMPOSIUM ON THE FOUNDATIONS OF SOFTWARE ENGINEERING (FSE 2014), 2014, : 791 - 794
  • [37] A numerical study to investigate the heat transfer and thermodynamic performance of a natural convection driven thermal energy storage system
    Satbhai, Ojas
    Roy, Subhransu
    Ghosh, Sudipto
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2017 VOL 8, 2018,
  • [38] Improved Speed Skating Performance at Altitude is Overestimated by Energy Flow Model
    Heine, Martin
    de Koning, Jos J.
    Noordhof, Dionne A.
    Foster, Carl
    MEDICINE AND SCIENCE IN SPORTS AND EXERCISE, 2010, 42 (05): : 784 - 784
  • [39] A changeable boundary prescribed performance control for the altitude ground test facility
    Lun, Yuebin
    Wang, Honglun
    Wu, Tiancai
    Zhang, Menghua
    Qian, Qiumeng
    NONLINEAR DYNAMICS, 2024, 112 (06) : 4409 - 4433
  • [40] A changeable boundary prescribed performance control for the altitude ground test facility
    Yuebin Lun
    Honglun Wang
    Tiancai Wu
    Menghua Zhang
    Qiumeng Qian
    Nonlinear Dynamics, 2024, 112 : 4483 - 4506
12345