| 摘要 |
<p>An aerospace control arrangement comprising a control unit (10) connected to a plurality of connecting node sets (20a, 20b, 20c), each connecting node set (20a, 20b, 20c) having associated therewith a plurality of connecting nodes (20), and each node (20) having associated therewith at least one effecter (24) and/or sensor (28), resulting in at least some of the nodes (20) being connected to the control unit (10) in a fault isolated star, point to point, arrangement.
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