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[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)
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