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Multi-Axis Independent Electromechanical Load Control for Docking System Actuation Development and Verification Using dSPACEThe development of highly complex and advanced actuation systems to meet customer demands has accelerated as the use of real-time testing technology expands into multiple markets at Moog. Systems developed for the autonomous docking of human rated spacecraft to the International Space Station (ISS), envelope multi-operational characteristics which place unique constraints on an actuation system. Real-time testing hardware has been used as a platform for incremental testing and development for the linear actuation system which controls initial capture and docking for vehicles visiting the ISS. This presentation will outline the role of dSPACE hardware as a platform for rapid control-algorithm prototyping as well as an Electromechanical Actuator (EMA) system dynamic loading simulator, both conducted at Moog to develop the safety critical Linear Actuator System (LAS) of the NASA Docking System (NDS).
Document ID
20150018599
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Oesch, Christopher
(Moog, Inc. East Aurora, NY, United States)
Dick, Brandon
(Boeing Space and Communications Huntsville, AL, United States)
Rupp, Timothy
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
October 1, 2015
Publication Date
October 13, 2015
Subject Category
Mechanical Engineering
Spacecraft Design, Testing And Performance
Electronics And Electrical Engineering
Report/Patent Number
JSC-CN-34400
Meeting Information
Meeting: dSPACE Technology Conference
Location: Plymouth, MI
Country: United States
Start Date: October 13, 2015
End Date: October 14, 2015
Sponsors: dSPACE, Inc.
Funding Number(s)
PROJECT: ISS NDSB1 Project (CR13642)
Distribution Limits
Public
Copyright
Public Use Permitted.
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