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@ -79,9 +79,31 @@ float ECL_PitchController::control(float pitch_setpoint, float pitch, float pitc
@@ -79,9 +79,31 @@ float ECL_PitchController::control(float pitch_setpoint, float pitch, float pitc
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airspeed = airspeed_min; |
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} |
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/* flying inverted (wings upside down) ? */ |
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bool inverted = false; |
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/* roll is used as feedforward term and inverted flight needs to be considered */ |
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if (fabsf(roll) < math::radians(90.0f)) { |
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/* not inverted, but numerically still potentially close to infinity */ |
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roll = math::constrain(roll, math::radians(-80.0f), math::radians(80.0f)); |
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} else { |
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/* inverted flight, constrain on the two extremes of -pi..+pi to avoid infinity */ |
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/* note: the ranges are extended by 10 deg here to avoid numeric resolution effects */ |
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if (roll > 0.0f) { |
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/* right hemisphere */ |
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roll = math::constrain(roll, math::radians(100.0f), math::radians(180.0f)); |
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} else { |
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/* left hemisphere */ |
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roll = math::constrain(roll, math::radians(-100.0f), math::radians(-180.0f)); |
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} |
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} |
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/* calculate the offset in the rate resulting from rolling */ |
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float turn_offset = fabsf((CONSTANTS_ONE_G / airspeed) * |
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tanf(roll) * sinf(roll)) * _roll_ff; |
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if (inverted) |
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turn_offset = -turn_offset; |
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float pitch_error = pitch_setpoint - pitch; |
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/* rate setpoint from current error and time constant */ |
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