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Autonomous docking ground demonstrationThe Autonomous Docking Ground Demonstration is an evaluation of the laser sensor system to support the docking phase (12 ft to contact) when operated in conjunction with the guidance, navigation, and control (GN&C) software. The docking mechanism being used was developed for the Apollo/Soyuz Test Program. This demonstration will be conducted using the 6-DOF Dynamic Test System (DTS). The DTS simulates the Space Station Freedom as the stationary or target vehicle and the Orbiter as the active or chase vehicle. For this demonstration, the laser sensor will be mounted on the target vehicle and the retroflectors will be on the chase vehicle. This arrangement was chosen to prevent potential damage to the laser. The laser sensor system, GN&C, and 6-DOF DTS will be operated closed-loop. Initial conditions to simulate vehicle misalignments, translational and rotational, will be introduced within the constraints of the systems involved.
Document ID
19930012241
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lamkin, Steve L.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Le, Thomas Quan
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Othon, L. T.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Prather, Joseph L.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Eick, Richard E.
(TRW, Inc. Houston, TX., United States)
Baxter, Jim M.
(TRW, Inc. Houston, TX., United States)
Boyd, M. G.
(Lockheed Engineering and Sciences Co. Houston, TX., United States)
Clark, Fred D.
(Lockheed Engineering and Sciences Co. Houston, TX., United States)
Spehar, Peter T.
(Lockheed Engineering and Sciences Co. Houston, TX., United States)
Teters, Rebecca T.
(Lockheed Engineering and Sciences Co. Houston, TX., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Washington, NASA Automated Rendezvous and Capture Review. Executive Summary
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N21430
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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