pc_req - CDIO-3 Product Concept Requirements Team Oscar...

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CDIO-3 Product Concept Requirements Team Oscar Murillo Leah Soffer Maggie Sullivan February 21, 2002
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Mission Statement Project Mission: Demonstrate the feasibility of electromagnetic control for formation flying satellites. Implications: ± Demonstrate ± EM Control ± Formation maneuvering vehicles
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Functional Requirements 1: the Customer Formation flying ± Stability in formation ± Interchangeable/replaceable modules ± Both autonomy and command response EM control ± “Use magnets to generate the … restoring forces” ± “… will allow between 3 and 6 DoF EMFF” Architectural notes ± High-permeability lightweight solenoid cores ± Necessary heat dissipation ± Reaction wheels
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Functional Requirements 2: the System Top-Level: “The system shall…” ± Have interchangeable system modules ± Be tested on a realistic facility ± Maintain relative separation/attitude ± Follow steady course, predetermined or MC Subsystems Power Flight computer ADS – Sensing ACS - Control Communication Protection Testing Integration
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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_req - CDIO-3 Product Concept Requirements Team Oscar...

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