Development of integrated orbit and attitude hardware-in-the-loop simulator system for satellite formation flying

Han Earl Park, Sang Young Park, Sung Woo Kim, Chandeok Park

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The development of an integrated orbit and attitude hardware-in-the-loop simulator (HILS) system for autonomous satellite formation flying is presented here. The integrated simulator system consists of an orbit HILS based on a GPS simulator and an attitude HILS based on a 3-DOF table-top air-bearing system and performs four processes (orbit determination, orbit control, attitude determination, and attitude control) which interact with each other in the same manner as actual flight processes do. Orbit determination is conducted by a relative navigation algorithm using double-difference GPS measurements and an extended Kalman filter (EKF). Orbit control uses a sub-optimal state-dependent Riccati equation (SDRE) technique. Attitude is determined from an AHRS sensor, and a PD feedback controller is used to control the attitude HILS via three momentum wheel assemblies. An integrated HIL simulation is performed for a formation reconfiguration scenario in which a deputy satellite moves from planar motion with a 500m baseline to coplanar motion with a 1,000 m baseline. By performing the four processes adequately, a 3D RMS position accuracy of 5.428 mm is achieved for relative navigation, and the deputy satellite successfully arrives at the target reconfiguration position with an accuracy of 2.598 m. Consequently, the performance of the integrated HILS and the feasibility of the applied determination/control algorithms are demonstrated by the integrated HIL simulation. The integrated simulator system developed here thus provides a ground-based testbed for realistic orbit/attitude coupled simulations of satellite formation flying missions. It can also be used as a basis for the future development of a hardware testbed for satellite formation flying technologies.

Original languageEnglish
Title of host publicationAstrodynamics 2013 - Advances in the Astronautical Sciences
Subtitle of host publicationProceedings of the AAS/AIAA Astrodynamics Specialist Conference
PublisherUnivelt Inc.
Pages3097-3116
Number of pages20
ISBN (Print)9780877036050
Publication statusPublished - 2014 Jan 1
Event2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013 - Hilton Head Island, SC, United States
Duration: 2013 Aug 112013 Aug 15

Publication series

NameAdvances in the Astronautical Sciences
Volume150
ISSN (Print)0065-3438

Other

Other2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013
CountryUnited States
CityHilton Head Island, SC
Period13/8/1113/8/15

    Fingerprint

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Park, H. E., Park, S. Y., Kim, S. W., & Park, C. (2014). Development of integrated orbit and attitude hardware-in-the-loop simulator system for satellite formation flying. In Astrodynamics 2013 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference (pp. 3097-3116). (Advances in the Astronautical Sciences; Vol. 150). Univelt Inc..