基于副气囊的平流层浮空器高度控制

doi:10.13700/j.bh.1001-5965.2020.0679

北京航空航天大学学报 ›› 2022, Vol. 48 ›› Issue (5): 762-770.doi: 10.13700/j.bh.1001-5965.2020.0679

基于副气囊的平流层浮空器高度控制

林康¹, 马云鹏¹, 郑泽伟², 武哲¹

1. 北京航空航天大学航空科学与工程学院, 北京 100083;
2. 北京航空航天大学自动化科学与电气工程学院, 北京 100083

收稿日期:2020-12-04 发布日期:2022-05-30
通讯作者: 马云鹏 E-mail:myp@buaa.edu.cn

Height control of stratospheric aerostat based on secondary airbag

LIN Kang¹, MA Yunpeng¹, ZHENG Zewei², WU Zhe¹

1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China;
2. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100083, China

Received:2020-12-04 Published:2022-05-30

摘要/Abstract

摘要： 浮空器悬停或飞行控制设计时，通常将风作为干扰项或阻力，螺旋桨需要消耗大量的能源克服风的阻力，而浮空器携带的能源有限，因此浮空器设计时存在欠能源问题。根据平流层风场的特点，采用副气囊控制浮空器的高度，实现平流层不同高度的风场利用，可以减小浮空器的能源消耗。建立浮空器高度控制模型，采用反步法设计浮空器高度控制器，利用状态观测器对浮空器的模型误差和输入误差进行估计，并进行了仿真分析，证明所设计的控制器能有效控制浮空器的高度。建立浮空器高度控制时其囊体内外压差变化模型，仿真分析表明,浮空器高度变化后，其囊体最终内外压差与初始压差相同。

关键词: 平流层浮空器, 副气囊, 高度控制, 风场利用, 反步法, 囊体内外压差

Abstract: In the past, when the aerostat hovering or flight control was designed, wind was used as an interference item or resistance, and the propeller was required to overcome the wind resistance. The energy carried by the aerostat is limited, so there is a problem of insufficient energy in the design of the aerostat.According to the characteristics of the stratospheric wind field, this paper uses a secondary airbag to control the height of the aerostat, realizes the utilization of wind fields with different heights in the stratosphere, and can reduce the energy consumption of the aerostat. In this paper, the aerostat height control model is established, backstepping is used to design the aerostat height controller, the state observer is used to estimate the aerostat model error and input error, and simulation analysis is performed to prove the designed controller can effectively control the height of the aerostat. And this paper establishes the change model of the pressure difference between the inside and outside of the airbag when the aerostat height is controlled, and simulates and analyzes the influence of the change of aerostat height on the pressure difference between the inside and outside of the airbag.

Key words: stratospheric aerostat, secondary airbag, height control, utilization of wind fields, backstepping, pressure difference between inside and outside of airbag

中图分类号:

V273

林康, 马云鹏, 郑泽伟, 武哲. 基于副气囊的平流层浮空器高度控制[J]. 北京航空航天大学学报, 2022, 48(5): 762-770.

LIN Kang, MA Yunpeng, ZHENG Zewei, WU Zhe. Height control of stratospheric aerostat based on secondary airbag[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(5): 762-770.

参考文献

[1] RONEY J A.Statistical wind analysis for near-space applications[J].Journal of Atmospheric and Solar-Terrestrial Physics,2007,69(13):1485-1501.
[2] YANG Y,WU J,ZHENG W.Design,modeling and control for a stratospheric telecommunication platform[J].Acta Astronautica,2012,80(6):181-189.
[3] GRACE D,MOHORCIC M.Broadband communications via high-altitude platforms[M].New York:John Wiley and Sons Ltd.,2011.
[4] MIURA R,SUZUKI M.Preliminary flight test program on telecom and broadcasting using high altitude platform station[J].Wireless Personal Communications,2003,24(2):341-361.
[5] GONZALO J,LÓPEZ D,DOMÍNGUEZ D,et al.On the capabilities and limitations of high-altitude pseudo-satellites[J].Progress in Aerospace Sciences,2018，98:37-56.
[6] D’OLIVEIRA F A,FRANCISCO C L D,TESSALENO C D.High-altitude platforms present situation and technology trends[J].Journal of Aerospace Technology and Management,2016,8(3):249-262.
[7] 赵达,刘东旭,孙康文,等.平流层飞艇研制现状、技术难点及发展趋势[J].航空学报,2016,37(1):45-56.ZHAO D,LIU D X,SUN K W,et al.Research status,technical difficulties and development trend of stratospheric airship[J].Acta Aeronautics et Astronautica Sinica,2016,37(1):45-56 (in Chinese).
[8] 陶梦初,何金海,刘毅.平流层准零风层统计特征及准两年周期振荡对其影响分析[J].气候与环境研究,2012,17(1):92-102.TAO M C,HE J H,LIU Y.Analysis of the characteristics of the stratospheric quasi-zero wind layer and the effects of quasi-biennial oscillation on it[J].Climatic and Environmental Research,2012,17(1):92-102(in Chinese).
[9] BELMONT A D,DARTT D G,NASTROM G D.Variations of stratospheric zonal winds,20-65 km,1961-1971[J].Journal of Applied Meteorology,1975,14(4):585-594.
[10] WANG G.Low stratospheric zero wind layer measurement with rayleigh doppler lidar[C]//International Symposium on Photoelectronic Detection and Imaging.Piscataway:IEEE Press,2013:890-504.
[11] BRADFORD L W,ROBERTS L C.Improved models of upper-level wind for several astronomical observatories[J].Physics,2010,19(2):820-837.
[12] FESEN R,BROWN Y.A method for establishing a long duration,stratospheric platform for astronomical research[J].Experimental Astronomy,2015,39(3):475-493.
[13] XU M,HUO W.Orbit control of a stratospheric satellite with parameter uncertainties[J].Advances in Space Research,2016,58(11):2341-2351.
[14] 符文星, 朱苏朋,闫杰,等.平流层卫星轨道控制系统研究[J].宇航学报,2008,29(5):1480-1484.FU W X,ZHU S P,YAN J,et al.Orbit control system for stratospheric satellite[J].Journal of Astronautics,2008,29(5):1480-1484(in Chinese).
[15] AARON K M,HEUN M K,NOCK K T.A method for balloon trajectory control[J].Advances in Space Research,2002,30(5):1227-1232.
[16] VANDERMEULEN I,GUAY M,MCLELLAN P J.Formation control of high-altitude balloons by distributed extremum seeking control[C]//American Control Conference.Piscataway:IEEE Press,2016:2524-2529.
[17] VANDERMEULEN I,GUAY M,MCLELLAN P J.Distributed control of high-altitude balloon formation by extremum-seeking control[J].IEEE Transactions on Control Systems Technology,2018,26(3):857-873.
[18] LIN K,ZHENG Z,WU Z,et al.Path following of a stratospheric satellite by the aid of wind currents[J].Proceedings of the Institution of Mechanical Engineers,2019,233(11):3983-4003.
[19] 邓小龙, 李魁,于春锐,等.准零风层新型临近空间浮空器区域驻留性能[J].国防科技大学学报,2019,41(1):5-12.DENG X L,LI K,YU C R,et al.Station-keeping performance of novel near-space aerostat in quasi-zero wind layer[J].Journal of National University of Defense Technology,2019,41(1):5-12(in Chinese).
[20] CHEN W H,YANG J,GUO L,et al.Disturbance-observer-based control and related methods an overview[J].IEEE Transactions on Industrial Electronics,2016,63(2):1083-1095.
[21] HU J,ZHANG H.Immersion and invariance based command-filtered adaptive backstepping control of VTOL vehicles[J].Automatica,2013,49(7):2160-2167.

基于副气囊的平流层浮空器高度控制

Height control of stratospheric aerostat based on secondary airbag

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