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@ -52,19 +52,21 @@ void QuadPlane::tailsitter_output(void)
@@ -52,19 +52,21 @@ void QuadPlane::tailsitter_output(void)
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if (!is_tailsitter()) { |
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return; |
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} |
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float tilt_left = 0.0f; |
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float tilt_right = 0.0f; |
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if (!tailsitter_active() || in_tailsitter_vtol_transition()) { |
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if (tailsitter.vectored_forward_gain > 0) { |
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// thrust vectoring in fixed wing flight
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float aileron = SRV_Channels::get_output_scaled(SRV_Channel::k_aileron); |
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float elevator = SRV_Channels::get_output_scaled(SRV_Channel::k_elevator); |
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float tilt_left = (elevator + aileron) * tailsitter.vectored_forward_gain; |
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float tilt_right = (elevator - aileron) * tailsitter.vectored_forward_gain; |
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tilt_left = (elevator + aileron) * tailsitter.vectored_forward_gain; |
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tilt_right = (elevator - aileron) * tailsitter.vectored_forward_gain; |
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} |
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SRV_Channels::set_output_scaled(SRV_Channel::k_tiltMotorLeft, tilt_left); |
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SRV_Channels::set_output_scaled(SRV_Channel::k_tiltMotorRight, tilt_right); |
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} else { |
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SRV_Channels::set_output_scaled(SRV_Channel::k_tiltMotorLeft, 0); |
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SRV_Channels::set_output_scaled(SRV_Channel::k_tiltMotorRight, 0); |
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} |
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if (in_tailsitter_vtol_transition() && !throttle_wait && is_flying() && hal.util->get_soft_armed()) { |
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/*
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during transitions to vtol mode set the throttle to the |
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@ -90,11 +92,10 @@ void QuadPlane::tailsitter_output(void)
@@ -90,11 +92,10 @@ void QuadPlane::tailsitter_output(void)
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tailsitter_speed_scaling(); |
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} |
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if (tailsitter.vectored_hover_gain > 0) { |
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// thrust vectoring VTOL modes
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float aileron = SRV_Channels::get_output_scaled(SRV_Channel::k_aileron); |
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float elevator = SRV_Channels::get_output_scaled(SRV_Channel::k_elevator); |
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tilt_left = SRV_Channels::get_output_scaled(SRV_Channel::k_tiltMotorLeft); |
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tilt_right = SRV_Channels::get_output_scaled(SRV_Channel::k_tiltMotorRight); |
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/*
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apply extra elevator when at high pitch errors, using a |
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power law. This allows the motors to point straight up for |
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@ -104,8 +105,8 @@ void QuadPlane::tailsitter_output(void)
@@ -104,8 +105,8 @@ void QuadPlane::tailsitter_output(void)
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float extra_pitch = constrain_float(pitch_error_cd, -4500, 4500) / 4500.0; |
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float extra_sign = extra_pitch > 0?1:-1; |
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float extra_elevator = extra_sign * powf(fabsf(extra_pitch), tailsitter.vectored_hover_power) * 4500; |
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float tilt_left = extra_elevator + (elevator + aileron) * tailsitter.vectored_hover_gain; |
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float tilt_right = extra_elevator + (elevator - aileron) * tailsitter.vectored_hover_gain; |
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tilt_left = extra_elevator + tilt_left * tailsitter.vectored_hover_gain; |
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tilt_right = extra_elevator + tilt_right * tailsitter.vectored_hover_gain; |
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if (fabsf(tilt_left) >= 4500 || fabsf(tilt_right) >= 4500) { |
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// prevent integrator windup
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motors->limit.roll_pitch = 1; |
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@ -217,9 +218,11 @@ void QuadPlane::tailsitter_speed_scaling(void)
@@ -217,9 +218,11 @@ void QuadPlane::tailsitter_speed_scaling(void)
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scaling = constrain_float(hover_throttle / throttle, 0, tailsitter.throttle_scale_max); |
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} |
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const SRV_Channel::Aux_servo_function_t functions[2] = { |
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const SRV_Channel::Aux_servo_function_t functions[4] = { |
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SRV_Channel::Aux_servo_function_t::k_aileron, |
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SRV_Channel::Aux_servo_function_t::k_elevator}; |
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SRV_Channel::Aux_servo_function_t::k_elevator, |
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SRV_Channel::Aux_servo_function_t::k_tiltMotorLeft, |
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SRV_Channel::Aux_servo_function_t::k_tiltMotorRight}; |
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for (uint8_t i=0; i<ARRAY_SIZE(functions); i++) { |
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int32_t v = SRV_Channels::get_output_scaled(functions[i]); |
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v *= scaling; |
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