Development of a Hardware-In-Loop (HIL) Simulator for Spacecraft Attitude Control Using Momentum Wheels

被引：0

作者：

Kim, Dohee ^{[1
]}

Park, Sang-Young ^{[1
]}

Kim, Jong-Woo ^{[2
]}

Choi, Kyu-Hong ^{[1
]}

机构：

[1] Yonsei Univ, Dept Astron, Astrodynam & Control Lab, Seoul 120749, South Korea

[2] Samsung Elect Co, Mechatron & Mfg Technol Ctr, Suwon 443742, South Korea

来源：

JOURNAL OF ASTRONOMY AND SPACE SCIENCES | 2008年 / 25卷 / 04期

关键词：

attitude control; hardware-in-the-loop simulator; momentum wheels; testbed;

D O I：

暂无

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

In this paper, a Hardware-In-the-Loop simulator to simulate attitude control of spacecraft using momentum wheels is developed. The simulator consists of a spherical air bearing system allowing rotation and tilt in all three axes, three momentum wheels for actuation, and an AHRS (Attitude Heading Reference System). The simulator processes various types of data in PC 104 and wirelessly communicates with a host PC using TCP/IP protocol. A simple low-cost momentum wheel assembly set and its drive electronics are also developed. Several experiments are performed to test the performance of the momentum wheels. For the control performance test of the simulator, a PID controller is implemented. The results of experimental demonstrations confirm the feasibility and validity of the Hardware-In-the-Loop simulator developed in the current study.

引用

页码：347 / 360

页数：14

共 50 条

[1] Development of a hardware-in-loop attitude control simulator for a CubeSat satellite
Tapsawat, Wittawat
Sangpet, Teerawat
Kuntanapreeda, Suwat
[J]. 8TH TSME-INTERNATIONAL CONFERENCE ON MECHANICAL ENGINEERING (TSME-ICOME 2017), 2018, 297
[2] Development of a Hardware-in-the-loop Simulator for Spacecraft Attitude Control Using Thrusters
Koh, Dong-Wook
Park, Sang-Young
Kim, Do-Hee
Choi, Kyu-Hong
[J]. JOURNAL OF ASTRONOMY AND SPACE SCIENCE, 2009, 26 (01) : 47 - 58
[3] Design and Development of Hardware-in-Loop Simulation of Spacecraft Attitude Control System Based on Wireless Ad Hoc Networking
Gao, Yudong
Wu, Jinjie
Hu, Min
Zheng, Wei
[J]. 2012 INTERNATIONAL CONFERENCE ON INDUSTRIAL CONTROL AND ELECTRONICS ENGINEERING (ICICEE), 2012, : 584 - 587
[4] Attitude Control of Spacecraft Simulator with Reaction Wheels Regulation
Malekzadeh, Maryam
Sadeghian, Hamid
[J]. 2017 5TH RSI INTERNATIONAL CONFERENCE ON ROBOTICS AND MECHATRONICS (ICROM 2017), 2017, : 101 - 106
[5] Spacecraft attitude control by 2 wheels with initial angular momentum
Katsuyama, Yuki
Sekiguchi, Kazuma
Sampei, Mitsuji
[J]. 2013 PROCEEDINGS OF SICE ANNUAL CONFERENCE (SICE), 2013, : 1890 - 1895
[6] Research on Benchmarking of Smart Camera Based on Hardware-in-Loop (HiL)
Zhao, Shuai
Zhang, Lu
Shen, Yongwang
Zhai, Yang
[J]. PROCEEDINGS OF 2020 IEEE 4TH INFORMATION TECHNOLOGY, NETWORKING, ELECTRONIC AND AUTOMATION CONTROL CONFERENCE (ITNEC 2020), 2020, : 1819 - 1823
[7] Development of a hardware simulator for the attitude estimation of a spacecraft on the ground test
Yamamoto, Takayuki
Miyazaki, Kanta
Tsujita, Katsuyoshi
[J]. 2022 61ST ANNUAL CONFERENCE OF THE SOCIETY OF INSTRUMENT AND CONTROL ENGINEERS (SICE), 2022, : 405 - 410
[8] Study on the Control System of a Hardware-in-Loop Micro-Satellite Simulator
Wang, Qian
Zhang, Tao
Song, Jingyan
[J]. 2009 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND BIOMIMETICS (ROBIO 2009), VOLS 1-4, 2009, : 2427 - 2432
[9] Applied nonlinear control of spacecraft simulator with constraints on torque and momentum of reaction wheels
Jamshidi, Somayeh
Mirzaei, Mehdi
Malekzadeh, Maryam
[J]. ISA TRANSACTIONS, 2023, 138 : 705 - 719
[10] An Online Hardware-in-the-Loop Testbed for Spacecraft Attitude Control
Bohlouri, Vahid
Hosseini-Onari, Hadi
Meibody, Mohammad N. P.
Seyedzamani, Soheil
[J]. 2019 27TH IRANIAN CONFERENCE ON ELECTRICAL ENGINEERING (ICEE 2019), 2019, : 1002 - 1006

← 1 2 3 4 5 →