APPARATUS FOR SIMULATING AIRCRAFT CONTROL LOADING
An electro-mechanical system for providing an opposing force to movement of a simulated control member in a grounded flight trainer. The invention utilizes an electric motor connected to the control member by a flexible element which, in the disclosed embodiment, comprises a continuous cable with a...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
22.01.1974
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Subjects | |
Online Access | Get full text |
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Summary: | An electro-mechanical system for providing an opposing force to movement of a simulated control member in a grounded flight trainer. The invention utilizes an electric motor connected to the control member by a flexible element which, in the disclosed embodiment, comprises a continuous cable with a predetermined amount of slack. This allows some degree of differential movement between the control member and motor, to which a pair of position potentiometers are respectively connected, thereby converting the differential position to an electrical signal which is used, together with other factors, to control movement of the motor. |
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Bibliography: | Application Number: CA19710103181 |