|
|
|
|
|
by jcalvinowens
275 days ago
|
|
> I think a big part of it, historically, is that this control scheme provides negative feedback > Think about the inertia of the pilot and their limbs inside the plane, acting on the controls. A sudden acceleration/jerk in the direction of the control signal will bias the operator's body to input the opposite control signal unless they are tensed up and prepared to maintain it in spite of the forces they experience. That is completely backwards, sorry. If the nose pitches up suddenly, the pilot tends to fall backwards, downhill. If the pilot holds the yoke like a handle, he commands further pitch up, which causes him to fall backwards more... The opposite is also true: a sudden pitch down causes an unrestrained pilot to fall forward onto the controls, commanding further pitch down, and so on. |
|
Also, I'm talking about the planes where these control schemes were developed a century ago. In these, center of gravity and the aerodynamic center and the pilot were all relatively close to each other. This is different on some modern airliner where the pilot is perched far out in front of the wings.
In those old planes, a pitch or roll would literally rotate the plane around the pilot who momentarily continues in their original orientation. If you are sitting at your desk with hands on a keyboard and I suddenly pitch your desk up, your hands will push further into the keyboard rather than fall away. This is how the pilot would experience the sudden pitch-up as well.