Integrated orbit and attitude hardware-in-The-loop simulations for autonomous satellite formation flying

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

Research output: Contribution to journalArticle

8 Citations (Scopus)

Abstract

Development and experiment of an integrated orbit and attitude hardware-in-The-loop (HIL) simulator for autonomous satellite formation flying are presented. The integrated simulator system consists of an orbit HIL simulator for orbit determination and control, and an attitude HIL simulator for attitude determination and control. The integrated simulator involves four processes (orbit determination, orbit control, attitude determination, and attitude control), which interact with each other in the same way as actual flight processes do. Orbit determination is conducted by a relative navigation algorithm using double-difference GPS measurements based on the extended Kalman filter (EKF). Orbit control is performed by a state-dependent Riccati equation (SDRE) technique that is utilized as a nonlinear controller for the formation control problem. Attitude is determined from an attitude heading reference system (AHRS) sensor, and a proportional-derivative (PD) feedback controller is used to control the attitude HIL simulator using three momentum wheel assemblies. Integrated orbit and attitude simulations are performed for a formation reconfiguration scenario. By performing the four processes adequately, the desired formation reconfiguration from a baseline of 500-1000 m was achieved with meter-level position error and millimeter-level relative position navigation. This HIL simulation demonstrates the performance of the integrated HIL simulator and the feasibility of the applied algorithms in a real-time environment. Furthermore, the integrated HIL simulator system developed in the current study can be used as a ground-based testing environment to reproduce possible actual satellite formation operations.

Original languageEnglish
Pages (from-to)2052-2066
Number of pages15
JournalAdvances in Space Research
Volume52
Issue number12
DOIs
Publication statusPublished - 2013 Dec 15

Fingerprint

hardware-in-the-loop simulation
formation flying
hardware
simulators
simulator
Orbits
Simulators
Satellites
orbits
Hardware
attitude control
Attitude control
simulation
navigation
controllers
Navigation
Riccati equation
position errors
orbit determination
Controllers

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Astronomy and Astrophysics
  • Geophysics
  • Atmospheric Science
  • Space and Planetary Science
  • Earth and Planetary Sciences(all)

Cite this

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abstract = "Development and experiment of an integrated orbit and attitude hardware-in-The-loop (HIL) simulator for autonomous satellite formation flying are presented. The integrated simulator system consists of an orbit HIL simulator for orbit determination and control, and an attitude HIL simulator for attitude determination and control. The integrated simulator involves four processes (orbit determination, orbit control, attitude determination, and attitude control), which interact with each other in the same way as actual flight processes do. Orbit determination is conducted by a relative navigation algorithm using double-difference GPS measurements based on the extended Kalman filter (EKF). Orbit control is performed by a state-dependent Riccati equation (SDRE) technique that is utilized as a nonlinear controller for the formation control problem. Attitude is determined from an attitude heading reference system (AHRS) sensor, and a proportional-derivative (PD) feedback controller is used to control the attitude HIL simulator using three momentum wheel assemblies. Integrated orbit and attitude simulations are performed for a formation reconfiguration scenario. By performing the four processes adequately, the desired formation reconfiguration from a baseline of 500-1000 m was achieved with meter-level position error and millimeter-level relative position navigation. This HIL simulation demonstrates the performance of the integrated HIL simulator and the feasibility of the applied algorithms in a real-time environment. Furthermore, the integrated HIL simulator system developed in the current study can be used as a ground-based testing environment to reproduce possible actual satellite formation operations.",
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Integrated orbit and attitude hardware-in-The-loop simulations for autonomous satellite formation flying. / Park, Han Earl; Park, Sang Young; Kim, Sung Woo; Park, Chandeok.

In: Advances in Space Research, Vol. 52, No. 12, 15.12.2013, p. 2052-2066.

Research output: Contribution to journalArticle

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