G - Physics – 05 – D
Patent
G - Physics
05
D
244/45, 341/83
G05D 1/00 (2006.01) B64C 13/46 (2006.01)
Patent
CA 1118516
ABSTRACT OF THE DISCLOSURE The present steering mechanism, especially for an aircraft includes a manually operable steering member and an automatic steering system. A difference signal formed from a pilot input and trim signal and from a gyro feedback signal is supplied to a force control and damping circuit twice, once directly and once through an authority limit circuit. The output of the authority limit circuit is also supplied to the motors forming part of the automatic steering system. The force con- trol and damping circuit also receives further input signal or signals representing steering information. The output of the force control and damping circuit is connected to the feed unit of the steering system, whereby an immediate manual control by the pilot is effective, however limited against an excessive control or so-called manual over control. 971/ar
322214
Gowling Lafleur Henderson Llp
Messerschmitt-Bolkow-Blohm Gmbh
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