Update Tuning.md

varadk2612 · web-flow · commit 29f4735b436f · 2024-04-11T16:49:20.000-05:00
diff --git a/docs/Electrical/Tuning.md b/docs/Electrical/Tuning.md
@@ -16,4 +16,6 @@ The PID controller has gains, or constant multipliers, corresponding to three ca
 
 *Derivative*: This gain is proportional to the derivative of the error. It contributes to a signal that is proportional to the instantaneous rate of change of error which it finds as the difference between the current and previous error.
 
+## Pitch tuning process
 
+For a fixed wing aircraft, tuning the pitch (nose up and down) might be the simplest because it is 

Original file line number	Diff line number	Diff line change
`@@ -16,4 +16,6 @@ The PID controller has gains, or constant multipliers, corresponding to three ca`
`16`	`16`
`17`	`17`	`Derivative: This gain is proportional to the derivative of the error. It contributes to a signal that is proportional to the instantaneous rate of change of error which it finds as the difference between the current and previous error.`
`18`	`18`
	`19`	`+## Pitch tuning process`
`19`	`20`
	`21`	`+For a fixed wing aircraft, tuning the pitch (nose up and down) might be the simplest because it is`