Chengdu J10-A

@TritonAerospace This is the discrete form of PID,discretization using backward difference method.Compared with continuous PID, discrete PID has better stability and adaptability in computer controlThe integral in this PID expression is the integral gain, which is the inverse of the integration time.

@York what equation are you using for your PID I've never seen such equation, I've used this exact way before to where 0 pitch commands PID to 0 Angular velocity but it is very very oscillate and will overshoot 0 every time & lower gains won't reach 0. is your PID heavy on the Integral?

@TritonAerospace The pitch is used as the input. PID is used to control the angular velocity to the set value. When the pitch is 0, the angular velocity is controlled to 0

how are you achieving zero angular velocity when you release all inputs?

@York 这两个都不是，降落的时候出了问题

@3639322358 飞控关了还是帧率低的原因？

@w2semail @w2semail 是猫咪

这个东西飞着飞着的时候容易失控

@GONDOR 那应该是图不准吧

另，我觉得腹部的进气道很还原，但是机头太胖了。您是照着线图做的？这个机头建议改改

歼十在腰部靠后位置有四片小减速板

@TritonAerospace Thank you. Yes, it's very convenient

very good, i really like your approach with flight control, first make centralized PID then pitch yaw roll each have a dedicated loop linked with main pid , and ability to switch off fc & good use of lists my next generation flight control is gonna be something similar.

@w2semail Ｏ(≧∇≦)Ｏ

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