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A dynamic motion simulator for future European docking systemsEurope's first confrontation with docking in space will require extensive testing to verify design and performance and to qualify hardware. For this purpose, a Docking Dynamics Test Facility (DDTF) was developed. It allows reproduction on the ground of the same impact loads and relative motion dynamics which would occur in space during docking. It uses a 9 degree of freedom, servo-motion system, controlled by a real time computer, which simulates the docking spacecraft in a zero-g environment. The test technique involves and active loop based on six axis force and torque detection, a mathematical simulation of individual spacecraft dynamics, and a 9 degree of freedom servomotion of which 3 DOFs allow extension of the kinematic range to 5 m. The configuration was checked out by closed loop tests involving spacecraft control models and real sensor hardware. The test facility at present has an extensive configuration that allows evaluation of both proximity control and docking systems. It provides a versatile tool to verify system design, hardware items and performance capabilities in the ongoing HERMES and COLUMBUS programs. The test system is described and its capabilities are summarized.
Document ID
19900012769
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brondino, G.
(Centre National d'Etudes Spatiales Toulouse (France)., United States)
Marchal, PH.
(Centre National d'Etudes Spatiales Toulouse (France)., United States)
Grimbert, D.
(MATRA Service Aerodynamique Velizy-Villacoublay (France)., United States)
Noirault, P.
(MATRA Espace Paris-Velizy, France)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Publication Information
Publication: NASA, John F. Kennedy Space Center, The 24th Aerospace Mechanisms Symposium
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
90N22085
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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