Abstract
The Middeck Active Control Experiment (MACE) was designed as a Space Shuttle flight experiment to be used to demonstrate high authority active structural control in zero gravity (0-g) conditions based on analysis, ground testing, and on-orbit control redesign. MACE is a multidisciplinary project which is at the forefront of flexible structural control. MACE was flown on STS-67 in March 1995, and this paper introduces a session devoted to the results of the mission.
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