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https://github.com/PX4/PX4-Autopilot.git
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wind estimator: added airspeed and sideslip gate sizes for innovation tests
Signed-off-by: Roman <bapstroman@gmail.com>
This commit is contained in:
@@ -93,7 +93,9 @@ private:
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(ParamFloat<px4::params::WEST_W_P_NOISE>) wind_p_noise,
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(ParamFloat<px4::params::WEST_SC_P_NOISE>) tas_scale_p_noise,
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(ParamFloat<px4::params::WEST_TAS_NOISE>) tas_noise,
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(ParamFloat<px4::params::WEST_BETA_NOISE>) beta_noise
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(ParamFloat<px4::params::WEST_BETA_NOISE>) beta_noise,
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(ParamInt<px4::params::WEST_TAS_GATE>) airspeed_gate,
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(ParamInt<px4::params::WEST_BETA_GATE>) sideslip_gate
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)
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static void cycle_trampoline(void *arg);
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@@ -274,6 +276,8 @@ void WindEstimatorModule::update_params()
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_wind_estimator.set_tas_scale_p_noise(tas_scale_p_noise.get());
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_wind_estimator.set_tas_noise(tas_noise.get());
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_wind_estimator.set_beta_noise(beta_noise.get());
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_wind_estimator.set_tas_gate(airspeed_gate.get());
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_wind_estimator.set_beta_gate(sideslip_gate.get());
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}
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int WindEstimatorModule::custom_command(int argc, char *argv[])
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@@ -36,3 +36,27 @@ PARAM_DEFINE_FLOAT(WEST_TAS_NOISE, 1.4);
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* @group Wind Estimator
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*/
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PARAM_DEFINE_FLOAT(WEST_BETA_NOISE, 0.3);
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/**
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* Gate size for true airspeed fusion.
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*
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* Sets the number of standard deviations used by the innovation consistency test.
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*
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* @min 1
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* @max 5
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* @unit SD
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* @group Wind Estimator
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*/
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PARAM_DEFINE_INT32(WEST_TAS_GATE, 3);
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/**
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* Gate size for true sideslip fusion.
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*
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* Sets the number of standard deviations used by the innovation consistency test.
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*
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* @min 1
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* @max 5
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* @unit SD
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* @group Wind Estimator
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*/
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PARAM_DEFINE_INT32(WEST_BETA_GATE, 1);
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