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@ -57,9 +57,9 @@ public:
@@ -57,9 +57,9 @@ public:
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} |
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// pid accessors
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AC_PID& get_rate_roll_pid() { return _pid_rate_roll; } |
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AC_PID& get_rate_pitch_pid() { return _pid_rate_pitch; } |
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AC_PID& get_rate_yaw_pid() { return _pid_rate_yaw; } |
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AC_PID& get_rate_roll_pid() override { return _pid_rate_roll; } |
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AC_PID& get_rate_pitch_pid() override { return _pid_rate_pitch; } |
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AC_PID& get_rate_yaw_pid() override { return _pid_rate_yaw; } |
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// passthrough_bf_roll_pitch_rate_yaw - roll and pitch are passed through directly, body-frame rate target for yaw
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void passthrough_bf_roll_pitch_rate_yaw(float roll_passthrough, float pitch_passthrough, float yaw_rate_bf_cds) override; |
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@ -72,7 +72,7 @@ public:
@@ -72,7 +72,7 @@ public:
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// rate_controller_run - run lowest level body-frame rate controller and send outputs to the motors
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// should be called at 100hz or more
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virtual void rate_controller_run(); |
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virtual void rate_controller_run() override; |
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// Update Alt_Hold angle maximum
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void update_althold_lean_angle_max(float throttle_in) override; |
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@ -143,7 +143,7 @@ private:
@@ -143,7 +143,7 @@ private:
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int16_t _passthrough_yaw; |
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// get_roll_trim - angle in centi-degrees to be added to roll angle. Used by helicopter to counter tail rotor thrust in hover
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float get_roll_trim_rad() { return constrain_float(radians(_hover_roll_trim_scalar * _hover_roll_trim * 0.01f), -radians(10.0f),radians(10.0f));} |
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float get_roll_trim_rad() override { return constrain_float(radians(_hover_roll_trim_scalar * _hover_roll_trim * 0.01f), -radians(10.0f),radians(10.0f));} |
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// internal variables
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float _hover_roll_trim_scalar = 0; // scalar used to suppress Hover Roll Trim
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