NASA NTRS · 20150018599
Multi-Axis Independent Electromechanical Load Control for Docking System Actuation Development and Verification Using dSPACE
Abstract
The 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).
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Oesch, Christopher, Dick, Brandon, Rupp, Timothy. 2015-10-13. Multi-Axis Independent Electromechanical Load Control for Docking System Actuation Development and Verification Using dSPACE. https://ntrs.nasa.gov/citations/20150018599
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