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https://github.com/paparazzi/paparazzi.git
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ce7fe4c23f
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)
22 lines
629 B
XML
22 lines
629 B
XML
<!DOCTYPE module SYSTEM "module.dtd">
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<module name="stabilization_passthrough" dir="stabilization" task="control">
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<doc>
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<description>
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Passthrough controller for rotorcraft
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</description>
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</doc>
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<dep>
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<depends>stabilization_rotorcraft,@attitude_command</depends>
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<provides>commands</provides>
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</dep>
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<header>
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<file name="stabilization_attitude_passthrough.h"/>
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</header>
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<makefile target="ap|nps" firmware="rotorcraft">
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<file name="stabilization_attitude_passthrough.c" dir="$(SRC_FIRMWARE)/stabilization"/>
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<define name="STABILIZATION_ATTITUDE_NO_REF"/>
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</makefile>
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</module>
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