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FixedwingPositionControl: fix air_gnd_angle judgement condition.
air_gnd_angle is from acos(), and never return a value that bigger than M_PI_F
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@ -658,7 +658,7 @@ FixedwingPositionControl::control_position(const math::Vector<2> &curr_pos, cons
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float air_gnd_angle = acosf((air_speed_2d * ground_speed) / (air_speed_2d.length() * ground_speed.length()));
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// if angle > 90 degrees or groundspeed is less than threshold, replace groundspeed with airspeed projection
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if ((fabsf(air_gnd_angle) > M_PI_F) || (ground_speed.length() < 3.0f)) {
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if ((fabsf(air_gnd_angle) > M_PI_2_F) || (ground_speed.length() < 3.0f)) {
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nav_speed_2d = air_speed_2d;
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} else {
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