A method and system for visually guiding an aircraft in its landing approach to a runway having an approach area equipped with approach lights operable in off, low, medium, and high intensity states. The lights are communicated with a secondary side of a transformer, which has a primary side with low, medium, and high taps that correspond to the light states. Off, low, medium, and high lighting intensity requests correspond to the low, medium, and high states of the plurality of lights. AC power is switched between the transformer taps in response to a request for an increase in lighting intensity. Power is sequentially applied to the taps by supplying the power to the low tap for a first predetermined time interval before supplying the power to the medium tap.

 
Web www.patentalert.com

< Non-jamming, fail safe flight control system with non-symmetric load alleviation capability

< Device for the recognition of residual synchronization errors of multiple slats of flaps placed next to each other in aircraft

> Inertial position target measuring systems and methods

> Flexible airfoils and method

~ 00280