Journal of Astronomy and Space Sciences

  • 제25권4호
  • /
  • Pages.347-360
  • /
  • 2008
  • /
  • 2093-5587(pISSN)
  • /
  • 2093-1409(eISSN)
한국우주과학회 (The Korean Space Science Society)
권호 표지
DOI QR코드

DOI QR Code

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

  • Kim, Do-Hee (Astrodynamics and Control Lab., Dept. of Astronomy, Yonsei University) ;
  • Park, Sang-Young (Astrodynamics and Control Lab., Dept. of Astronomy, Yonsei University) ;
  • Kim, Jong-Woo (Mechatronics & Manufacturing Technology Center, Samsung Electronics Co.) ;
  • Choi, Kyu-Hong (Astrodynamics and Control Lab., Dept. of Astronomy, Yonsei University)
  • 발행 : 2008.12.15
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

In this paper, a Hardware-In-the-Loop simulator to simulate attitude control of space craft 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 PC104 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.

키워드

참고문헌

  1. Edwards, S., Lavagno, L., Lee, E. A., & Vincentelli, A. S. 1997, Proceedings of the IEEE, 85, 366
  2. Kim, B. M., Velenis, E., Kriengsiri, P., & Tsiotras, P. 2001, AIAA/AAS Astrodynamics Specialists Conference, AIAA 2001-367
  3. Kim, D. 2008, Master Thesis, Yonsei University
  4. Norton, R. L. 2006, Machine Design: An integrated approach, 3rd Ed. (New Jersey: Prentice Hall
  5. Penrose, R. 1955, Proceedings of the Cambridge Philosophical Society, 51, 406
  6. Schwartz, J. L., Peck, M. A., & Hall, C. D. 2003, JGCD, 26, 513 https://doi.org/10.2514/2.5085
  7. Tanygin, S. & Williams, T. 1997, JGCD, 20, 625 https://doi.org/10.2514/2.4099
  8. Wang, F., Cao, Xi-Bin, Yang, Y., & Gao, D. 2006, AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA 2006-6733

피인용 문헌

  1. Quaternion-based attitude control design and hardware-in-the-loop simulation of suborbital modules with cold gas thrusters vol.229, pp.4, 2015, https://doi.org/10.1177/0954410014539294
  2. Attitude control in spacecraft orbit-raising using a reduced quaternion model vol.1, pp.4, 2014, https://doi.org/10.12989/aas.2014.1.4.427
  3. Verification of a CubeSat via hardware-in-the-loop simulation vol.50, pp.4, 2014, https://doi.org/10.1109/TAES.2014.130370
  4. Hardware-In-the-Loop Simulations of spacecraft attitude synchronization using the State-Dependent Riccati Equation technique vol.51, pp.3, 2013, https://doi.org/10.1016/j.asr.2012.09.004