Control system of new micro-gravity experimental system "BOV" from high altitude balloon

被引:0
作者
Bonda, Nobutaka [1 ]
Sakai, Shin-ichiro [1 ]
Sawai, Shujiro [1 ]
Hashimoto, Tatsuaki [1 ]
机构
[1] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2298510, Japan
来源
AMC '08: 10TH INTERNATIONAL WORKSHOP ON ADVANCED MOTION CONTROL, VOLS 1 AND 2, PROCEEDINGS | 2008年
关键词
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper proposes control system for a new micro gravity experimental system called BOV (Balloon-based Operation Vehicle). BOV uses a free-fall capsule with doubleshell structure to prevent influence of aerodynamic disturbance. Additionally, BOV is raised to 40km by a high altitude balloon to extend micro gravity duration to 30(or possibly 60) seconds. Thus we realize a medium duration micro gravity experimental system with good micro gravity environment. In this system, the most characteristic point is double-shell Structure. The inner shell can fall freely since the outer shell is controlled not to collide with the inner shell. To realize this non-contact control, BOV's body is controlled by translational control and attitude control. For translational control, there are four laser displacement sensors in the middle of BOV to measure clearance between the inner shell and the outer shell. The center position of the inner shell is estimated by the Newton-Raphson method with four laser displacement sensors. Using this estimation, force commands are calculated with PD controller. Attitude control is also necessary to maintain stable micro gravity experiments. BOV has three fiber optical gyros to measure the body rates. Torque commands are also calculated with PD controller. The rolling angle is controlled by only D controller since the initial error angle is possible to exert a bad influence for that the balloon is rotated in the upper air. BOV is separated from the high altitude balloon after the balloon arrives at 40km altitude. For 35 seconds the micro gravity experiment is carried out. After the experiment, the pilot-chute is opened for speed reduction. In addition, main-chute is opened at 7.5km altitude for safety descent. In this paper, control system for the new micro gravity experimental system is proposed. This system has double shell structure and the inner shell can fall freely. In the experiment, we realize good-quality micro gravity and realize to continue moderate micro gravity duration. This system is now improving and near future we can utilize BOV's system for moderate micro gravity duration with low-cost easily.
引用
收藏
页码:590 / 594
页数:5
相关论文
共 50 条
[1]   Development of A Micro-gravity Experiment System Using A High Altitude Balloon [J].
Hashimoto, Tatsuaki ;
Sawai, Shujiro ;
Sakai, Shin'ichiro ;
Bando, Nobutat ;
Kobayashi, Hiroaki ;
Ishikawa, Takehiko ;
Inatomi, Yuko ;
Fujita, Kazuhisa ;
Yoshimitsu, Tctsuo ;
Saito, Yoshitaka ;
Fuke, Hidcyuki .
INTERNATIONAL JOURNAL OF MICROGRAVITY SCIENCE AND APPLICATION, 2009, 26 (01) :9-14
[2]   Drag-Free Control for Micro Gravity Experimental System with High Altitude Balloon [J].
Bando, Nobutaka ;
Sakai, Shin-ichiro ;
Sawai, Shujiro ;
Hoshino, Shinji ;
Tajima, Ken-ichi ;
Kadooka, Shouhei ;
Hashimoto, Tatsuaki ;
Ueno, Seiya ;
Soshi, Takahiro ;
Kobayashi, Hideaki ;
Fujita, Kazuhisa ;
Ishikawa, Takehiko ;
Inatomi, Yuko .
INTERNATIONAL JOURNAL OF MICROGRAVITY SCIENCE AND APPLICATION, 2009, 26 (01) :29-35
[3]   Micro-gravity environment generated by superconducting magnet system [J].
Key Laboratory of Condition Monitoring and Control for Power Plant Equipment, North China Electric Power University, Beijing 102206, China ;
不详 .
Zhongguo Dianji Gongcheng Xuebao, 2006, 22 (157-161)
[4]   Design of an active suspension system for a micro-gravity experiment [J].
Bergeon, B ;
Martinez, D ;
Coustal, P ;
Granier, JP .
CONTROL ENGINEERING PRACTICE, 1996, 4 (11) :1491-1502
[5]   Design and investigation of ground micro-gravity experimental system for large space spinning structures [J].
Wei, Guo ;
Sun, Jialiang ;
Li, Xinyuan ;
Guo, Jiaojiao ;
Jin, Dongping .
MECHANISM AND MACHINE THEORY, 2025, 205
[6]   Station-keeping performance analysis for high altitude balloon with altitude control system [J].
Du, Huafei ;
Lv, Mingyun ;
Li, Jun ;
Zhu, Weiyu ;
Zhang, Lanchuan ;
Wu, Yifei .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 :644-652
[7]   Payload System Development for High Altitude Balloon [J].
Kimm, Haklin .
2014 IEEE/SICE INTERNATIONAL SYMPOSIUM ON SYSTEM INTEGRATION (SII), 2014, :730-735
[8]   Recovery beacon system for high altitude balloon [J].
Hedqvist, T .
16TH ESA SYMPOSIUM ON EUROPEAN ROCKET AND BALLOON PROGRAMMES AND RELATED RESEARCH, PROCEEDINGS, 2003, 530 :217-221
[9]   Comparative Study of Impact of Compressor Speed on System Performance Subject to Micro-gravity [J].
Ma, Rui ;
Wu, Yu-ting ;
Du, Chun-xu ;
Chen, Xia ;
Zhang, De-lou ;
Ma, Chong-fang .
PROCEEDINGS OF 2016 7TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING, (ICMAE), 2016, :160-164
[10]   Ground Micro-gravity Emulation System for Space Robot Capturing the Target Satellite [J].
Yang, Haitao ;
Xie, Zongwu ;
Zhao, Xiaoyu ;
Jin, Minghe .
2015 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND BIOMIMETICS (ROBIO), 2015, :2585-2590