pc_dat - CDIO EMFF Test Bed CDIO Design Concept CDIO Space...

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CDIO EMFF Test Bed CDIO EMFF Test Bed Design Concept Design Concept CDIO Space Systems Product Development Databasing Team 21 February 2002 1
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Mission Objective Mission Objective z Demonstrate the feasibility of electromagnetic control for formation-flying satellites. z 2-D Flat floor test bed z 3 independent devices z 3 DOF per device Æ Simplifies problem while achieving objective Æ Proves feasibility of planar control Æ Simplifies dynamics Planar control vs. linear control… it takes 3 points to make a plane. Plus, if we can prove controllability for 3 devices, adding more should be… trivial… 2
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Requirements Requirements Flowdown Flowdown Simulated Solar Cells Power EM Shielding Actuation Reaction De-spin Inertial Metrology Separation distance Relative Metrology ACDS Carriage Frictionless mount Structure Ground Comm Omnidirectional Inter-device Comm Communication Power Amp On-board Computer Software Signal Conditioning Avionics Ground computer Human Controller Interface 20' x 30' Flat floor facility Operations Mission objective Separation distance: O(10cm)-O(1m) 3
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This note was uploaded on 11/08/2011 for the course AERO 16.810 taught by Professor Olivierdeweck during the Winter '07 term at MIT.

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pc_dat - CDIO EMFF Test Bed CDIO Design Concept CDIO Space...

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