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Howto:Implement a Fly-By-Wire System for Airliners: Difference between revisions
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Howto:Implement a Fly-By-Wire System for Airliners (view source)
Revision as of 09:58, 7 February 2012
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Another feature in the Boeing 787-8's Fly By Wire is the automatic control of the trailing edge camber which affects lift and drag. The fly-by-wire automatically adjusts that to get maximum efficiency. Redneck and I am working on that but it's not included in the below nasal code as I don't think any other aircraft has that. And ofcourse, it's not yet completed. The rest of the Fly-By-Wire is stable at the moment and has been tested on the new Boeing 787-8. | Another feature in the Boeing 787-8's Fly By Wire is the automatic control of the trailing edge camber which affects lift and drag. The fly-by-wire automatically adjusts that to get maximum efficiency. Redneck and I am working on that but it's not included in the below nasal code as I don't think any other aircraft has that. And ofcourse, it's not yet completed. The rest of the Fly-By-Wire is stable at the moment and has been tested on the new Boeing 787-8. | ||
== Note for Airbus Aircraft Developers == | |||
About Airbus Fly By Wire : [http://www.apollosoftware.com/products/FlyByWire/FlyByWire_english.pdf] | |||
I've just seen that the airbus Fly By Wire works slightly different. I'll create a new fly-by-wire / modify this one to have it function that way. In Airbus Aircraft, moving the control stick controls angular acceleration, and not angular velocity. That is, when you move the stick to the left, the plane starts turning left, when you bring the stick back to the center, the fly-by-wire asks the plane to maintain that bank angle. It's the same case for pitch, and this is not available in Boeing's Fly-By-Wire. | |||
== Functions == | == Functions == | ||