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An Educational Platform for Small Satellite Development with Proximity Operation CapabilitiesAn alternative to ground testing of small satellites is presented here, where the kinematics of a 3U underactuated CubeSat operating in 3 degrees-of-freedom (DOF) is reproduced by an omnidirectional wheeled platform, while satellite dynamics are simulated in real-time. The system is equipped with a relative navigation sensor in the form factor of a smartphone, the Smartphone Video Guidance Sensor (SVGS), allowing the platform to reproduce proximity operation maneuvers. The wheeled platform is used as an educational tool for students over a large range of academic levels, from high school to graduate school. A derivation of the kinematic relationship from satellite dynamics to rotacaster wheel velocities is presented, along with the guidance and control laws of the system. Simulation and experimental results demonstrate that the wheeled platform was able to successfully replicate detumble, slew, and attitude hold maneuvers of a 3U CubeSat.
Document ID
20180006366
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Bertaska, Ivan R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rakoczy, John
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
October 17, 2018
Publication Date
August 4, 2018
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
M18-6777
Meeting Information
Meeting: AIAA/USU Small Satellite Conference
Location: Logan, UT
Country: United States
Start Date: August 4, 2018
End Date: August 9, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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