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Compiling attitude control, ready for tests
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@@ -39,6 +39,11 @@
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#include "../ecl.h"
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#include "ecl_roll_controller.h"
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#include <stdint.h>
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#include <float.h>
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#include <geo/geo.h>
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#include <ecl/ecl.h>
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#include <mathlib/mathlib.h>
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ECL_RollController::ECL_RollController() :
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_last_run(0),
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@@ -61,7 +66,7 @@ float ECL_RollController::control(float roll_setpoint, float roll, float roll_ra
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float dt = (dt_micros > 500000) ? 0.0f : dt_micros / 1000000;
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float k_ff = max((_k_p - _k_i * _tc) * _tc - _k_d, 0.0f);
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float k_ff = math::max((_k_p - _k_i * _tc) * _tc - _k_d, 0.0f);
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float k_i_rate = _k_i * _tc;
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/* input conditioning */
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@@ -86,7 +91,7 @@ float ECL_RollController::control(float roll_setpoint, float roll, float roll_ra
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float ilimit_scaled = 0.0f;
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if (!lock_integrator && k_i_rate > 0.0f && airspeed > 0.5 * airspeed_min) {
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if (!lock_integrator && k_i_rate > 0.0f && airspeed > 0.5f * airspeed_min) {
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float id = _rate_error * k_i_rate * dt * scaler;
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@@ -96,21 +101,21 @@ float ECL_RollController::control(float roll_setpoint, float roll, float roll_ra
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*/
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if (_last_output < -_max_deflection_rad) {
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/* only allow motion to center: increase value */
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id = max(id, 0.0f);
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id = math::max(id, 0.0f);
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} else if (_last_output > _max_deflection_rad) {
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/* only allow motion to center: decrease value */
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id = min(id, 0.0f);
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id = math::min(id, 0.0f);
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}
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_integrator += id;
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}
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/* integrator limit */
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_integrator = constrain(_integrator, -ilimit_scaled, ilimit_scaled);
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_integrator = math::constrain(_integrator, -ilimit_scaled, ilimit_scaled);
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/* store non-limited output */
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_last_output = ((_rate_error * _k_d * scaler) + _integrator + (_rate_setpoint * k_roll_ff)) * scaler;
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_last_output = ((_rate_error * _k_d * scaler) + _integrator + (_rate_setpoint * k_ff)) * scaler;
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return constrain(_last_output, -_max_deflection_rad, _max_deflection_rad);
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return math::constrain(_last_output, -_max_deflection_rad, _max_deflection_rad);
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}
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void ECL_RollController::reset_integrator()
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