Design a Yaw Controller for a Toy Quad-Copter

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SUMMARY

This discussion focuses on designing a yaw controller for a toy quad-copter, specifically addressing the challenge of maintaining accurate yaw while the quad-copter is in motion. The user calculates the required yaw angle using trigonometry based on starting and destination coordinates, but encounters issues with the quad-copter's stability during rotation. The conversation emphasizes the interdependence of roll, pitch, and yaw, and highlights the importance of considering side slip in the control design. For further insights, a relevant resource on control loop tuning is provided.

PREREQUISITES
  • Understanding of quad-copter dynamics
  • Familiarity with trigonometric calculations for angle determination
  • Knowledge of control theory, particularly regarding roll, pitch, and yaw
  • Experience with programming for quad-copter flight control
NEXT STEPS
  • Study the principles of quad-copter flight dynamics
  • Learn about PID controllers and their application in quad-copter stabilization
  • Explore the ArduPilot documentation on roll-pitch controller tuning
  • Investigate methods for minimizing side slip during quad-copter maneuvers
USEFUL FOR

This discussion is beneficial for hobbyists and developers working on quad-copter flight control systems, particularly those interested in enhancing stability and precision in yaw control.

stosw
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I've been currently playing around with a toy quad-copter that you can write your own programs for and was attempting to make it go to a set of coordinates that are specified. I was wondering if someone could help me design a controller for the yaw component.

I am currently calculating the angle needed to turn by take the two points, starting and destination, and using a triangle to find the angle. This works great for a stationary object and turns to the desired angle. The problem comes from the toy not staying directly in place while rotating.

Any input would be greatly appreciated.
 
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