Type: Conference Paper
Mechatronic design and construction of a five axes satellite simulator
Journal: ()Year: 24 March 2017Volume: Issue: Pages: 210 - 215
DOI:10.1109/ICRoM.2016.7886848Language: English
Abstract
This article describes the construction of a five spacecraft flight simulator based on an air bearing system, which was designed and instrumented in university of Isfahan laboratory to evaluate and to perform research in the field of Attitude Determination and Control Systems for spacecraft. This simulator is modeled in Autodesk-Inventor software package to design the simulator component precisely. The hardware and software components of the testbed are detailed in this article. the constraints for the construction and final realization of this attitude simulator testbed are depicted. It describes all modifications needed to reconfigure the simulator system testbed. © 2016 IEEE.
Author Keywords
Air Bearing SystemConstruction of a SimulatorFive Axes Spacecraft SimulatorHardware in the loop Verification
Other Keywords
Bearings (machine parts)Computer aided manufacturingFlight control systemsFlight simulatorsHardwareRoboticsSatellite simulatorsSimulatorsSpace simulatorsSpacecraftTestbedsAir bearing systemsAttitude determination and control systemHard-ware-in-the-loopHardware and software componentsMechatronic designSimulator componentsSimulator systemsSpacecraft simulatorsComputer software