Skip to content
New issue

Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.

By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.

Already on GitHub? Sign in to your account

[control] rework the stabilization for rotorcraft #3248

Merged
merged 1 commit into from
May 21, 2024

Commits on Apr 7, 2024

  1. [control] rework the stabilization for rotorcraft

    Introducing several changes to the control stask for the stabilization:
    - new structures: stabilization, stab (att and/or rates) and thrust (vector)
    - more functional approach: stabilization receives the stab and thrust
      setpoints from guidance and fill command vector at the end
    - modes and sub-modes are redefined (split stab and guidance modes),
      some AP modes are removed (FLIP and MODULE)
    - RC read functions are removed and replaced by ABI bindings, one for
      each part (AP, stab, guidance_h, guidance_v) with dedicated functions
    - transition ratio (float in [0-1]) replace transition_percentage (int)
    - the AP_MODULE mode is replaced by generated autopilot
    - the ABI hack for guidance indi is not needed anymore
    - AP generator supports a new 'store' attribute to use return values of
      functions
    - cleaning of the stabilization API (for setter functions)
    gautierhattenberger committed Apr 7, 2024
    Configuration menu
    Copy the full SHA
    0d42cd1 View commit details
    Browse the repository at this point in the history