Relationship between ROLL and YAW! | Understanding Roll due to Yaw & Yaw due to Roll & Steady Turns!

[@AndreaSSLeventiSS]

The rudder deflection in the first example should actually lead to a positive yawing motion, i.e. turn to the right. Good explanation!

[@JxJAVIATION]

Oh yes. I noticed it after reading the comments. My bad and apologies!

[@surideedesigns]

That's confused the hell out of me 😅

[@danielgimj]

This was very simple and helpful. Thank you!! 🙏

[@JxJAVIATION]

You're welcome! Check out my other videos as well!

[@argydimitrelis611]

Very nice as always

[@JxJAVIATION]

Thank you! Cheers!

[@c123bthunderpig]

Informative As always - new voice? Your videos are perfect length, I save them for a quick refresher guide.

[@JxJAVIATION]

Voice is the same actually! Thank you for watching and sending out your comments. Always brings a smile! :)

[@hari7049]

You said the yawing and rolling motion are interrelated. So what should be the postions of rudder and ailerons to do a yawing and rolling motion together. I am currently designing a paper airplane which can do both simultaneosly. Your answer can help me design it.

[@JxJAVIATION]

If the airplane has to yaw to the right, the rudder has to deflect towards the right, the right aileron should deflect down and left aileron up

[@pilot.sakshi]

Wow your videos are very helpful 😊👍 I always write down your every sentence explained in my book

[@JxJAVIATION]

That's awesome! I do a lot of research before making and publishing videos for the benefit of viewers like yourself. Keep Watching! Cheers!!

[@cravyvlogs1487]

I love your video! Thanks so much

[@JxJAVIATION]

You are so welcome!

[@ljs3878]

Learned a lot, and now I have a question. If roll and yaw movements are interrelated and happen simultaneously, why are they controlled independently by yoke and pedal? Is it to accelerate a specific movement in different situations? e.g. when you want to make a fast turn to the left, you step on the pedal instead of turning the yoke, yet aware that stability could decrease?

[@JxJAVIATION]

Well! You basically answered your question. In some cases only rudder inputs or only aileron inputs may be required, such as during a crosswind landing or incase of a lateral disturbance, which is why yoke and pedals are provided to control the surfaces separately.

[@ljs3878]

@JxJ AVIATION Now I get it all. Thanks for answering with great examples!

[@Quiseph64]

On a rotorcraft, the differences are much more obvious, too.

[@SOURAYANMISRA-p1u]

I still have a question on how the horizontal vector is causing the yaw, please can you explain in here...

[@JxJAVIATION]

What would be your question?

[@sirflabbyflabz]

in your explanation of yaw, wouldn't a rudder deflection to the right result in a yaw to the right and not left like in your video?

[@JxJAVIATION]

yes. animation was incorrect

[@scientifictech2816]

Bro which ILS support auto land? Does ILS CAT 1 and CAT 2 support autoland instead of ILS CAT 3?

[@JxJAVIATION]

For Auto Land ILS CAT 3 is required. The others do not support Auto Land

[@RajeevKumar-mu2cj]

Excellent

[@JxJAVIATION]

Thank you! Do check out my other videos as well!

[@markmorose]

Ooohhhhh, first video that explained it to me right lol

[@JxJAVIATION]

Thank you! Check out my other videos as well!

[@johnnoonan5802]

bring up yaw dampers as well im sure there are folk who have never heard of yaw dampers and their significance ,, thank you JxJ

[@JxJAVIATION]

Thank you for watching!! Please do check out my other videos as well!

[@khanhvocnhua4517]

+1 step to the pilot dream... but idk how many step are there =((

[@JxJAVIATION]

There are many steps in this journey. Videos in my channel should help you in that journey.

[@mrlitespeed]

Haha. How you expect viewers to understand roll and yaw and their interconnection, when you yourself don't understand it ? The tilt of the resulting airforce vector (not just the lift vector) causes the plane to slide towards the hanging wing. (And being now unbalanced with the weight vector causes the plane also to accelerate downwards.) The yaw - the 'adverse' yaw as it's called in the biz - is caused by the uneven induced drag the ailerons produce upon being deflected. You can't properly explain adverse yaw without introducing and explaining the term induced drag beforehand.

[@JxJAVIATION]

cool thanks for the input