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synced 2026-10-14 04:13:33 +08:00
decreased filter cutoff frequenmcy to 5Hz, nocoscillations
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@@ -179,7 +179,7 @@ PARAM_DEFINE_FLOAT(C_D2, 1.984f);
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* @increment 0.0001
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* @group FW DYN SOAR Control
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*/
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PARAM_DEFINE_FLOAT(FILTER_A1, 0.53010968f);
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PARAM_DEFINE_FLOAT(FILTER_A1, 1.16826067f);
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/**
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* coefficients of the butterworth filter used for smoothing the IMU
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@@ -191,7 +191,7 @@ PARAM_DEFINE_FLOAT(FILTER_A1, 0.53010968f);
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* @increment 0.0001
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* @group FW DYN SOAR Control
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*/
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PARAM_DEFINE_FLOAT(FILTER_A2, -0.22169409f);
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PARAM_DEFINE_FLOAT(FILTER_A2, -0.42411821f);
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/**
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* coefficients of the butterworth filter used for smoothing the IMU
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@@ -203,7 +203,7 @@ PARAM_DEFINE_FLOAT(FILTER_A2, -0.22169409f);
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* @increment 0.0001
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* @group FW DYN SOAR Control
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*/
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PARAM_DEFINE_FLOAT(FILTER_B1, 0.1728961f);
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PARAM_DEFINE_FLOAT(FILTER_B1, 0.06396438f);
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/**
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* coefficients of the butterworth filter used for smoothing the IMU
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@@ -215,7 +215,7 @@ PARAM_DEFINE_FLOAT(FILTER_B1, 0.1728961f);
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* @increment 0.0001
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* @group FW DYN SOAR Control
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*/
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PARAM_DEFINE_FLOAT(FILTER_B2, 0.3457922f);
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PARAM_DEFINE_FLOAT(FILTER_B2, 0.12792877f);
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/**
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* coefficients of the butterworth filter used for smoothing the IMU
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@@ -227,7 +227,7 @@ PARAM_DEFINE_FLOAT(FILTER_B2, 0.3457922f);
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* @increment 0.0001
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* @group FW DYN SOAR Control
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*/
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PARAM_DEFINE_FLOAT(FILTER_B3, 0.1728961f);
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PARAM_DEFINE_FLOAT(FILTER_B3, 0.06396438f);
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// ========================================================
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// =================== CONTROL GAINS ======================
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