Plane: : integrate AC_WPNav::get_speed rename to get_default_speed
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@ -970,7 +970,7 @@ bool QuadPlane::is_flying_vtol(void) const
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*/
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float QuadPlane::landing_descent_rate_cms(float height_above_ground) const
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{
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float ret = linear_interpolate(land_speed_cms, wp_nav->get_speed_down(),
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float ret = linear_interpolate(land_speed_cms, wp_nav->get_default_speed_down(),
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height_above_ground,
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land_final_alt, land_final_alt+6);
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return ret;
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@ -1146,7 +1146,7 @@ float QuadPlane::assist_climb_rate_cms(void) const
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climb_rate = plane.g.flybywire_climb_rate * (plane.nav_pitch_cd/(float)plane.aparm.pitch_limit_max_cd);
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climb_rate *= plane.get_throttle_input();
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}
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climb_rate = constrain_float(climb_rate, -wp_nav->get_speed_down(), wp_nav->get_speed_up());
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climb_rate = constrain_float(climb_rate, -wp_nav->get_default_speed_down(), wp_nav->get_default_speed_up());
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// bring in the demanded climb rate over 2 seconds
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const uint32_t ramp_up_time_ms = 2000;
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@ -1859,7 +1859,7 @@ void QuadPlane::vtol_position_controller(void)
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// approach
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// max_speed will control how fast we will fly. It will always decrease
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poscontrol.max_speed = MAX(speed_towards_target, wp_nav->get_speed_xy() * 0.01);
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poscontrol.max_speed = MAX(speed_towards_target, wp_nav->get_default_speed_xy() * 0.01);
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poscontrol.speed_scale = poscontrol.max_speed / MAX(distance, 1);
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}
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@ -2081,7 +2081,7 @@ void QuadPlane::takeoff_controller(void)
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plane.nav_pitch_cd,
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get_pilot_input_yaw_rate_cds() + get_weathervane_yaw_rate_cds());
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pos_control->set_alt_target_from_climb_rate(wp_nav->get_speed_up(), plane.G_Dt, true);
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pos_control->set_alt_target_from_climb_rate(wp_nav->get_default_speed_up(), plane.G_Dt, true);
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run_z_controller();
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}
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@ -2440,7 +2440,7 @@ int8_t QuadPlane::forward_throttle_pct(void)
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// add in a component from our current pitch demand. This tends to
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// move us to zero pitch. Assume that LIM_PITCH would give us the
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// WP nav speed.
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fwd_vel_error -= (wp_nav->get_speed_xy() * 0.01f) * plane.nav_pitch_cd / (float)plane.aparm.pitch_limit_max_cd;
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fwd_vel_error -= (wp_nav->get_default_speed_xy() * 0.01f) * plane.nav_pitch_cd / (float)plane.aparm.pitch_limit_max_cd;
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if (should_relax() && vel_ned.length() < 1) {
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// we may be landed
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