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heightrate p as parameter
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@@ -231,7 +231,7 @@ void TECS::_update_height_demand(float demand, float state)
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_hgt_dem_adj = demand;//0.025f * demand + 0.975f * _hgt_dem_adj_last;
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_hgt_dem_adj_last = _hgt_dem_adj;
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_hgt_rate_dem = (_hgt_dem_adj-state)*0.1f; //xxx: parameter
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_hgt_rate_dem = (_hgt_dem_adj-state)*_heightrate_p;
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// Limit height rate of change
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if (_hgt_rate_dem > _maxClimbRate) {
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_hgt_rate_dem = _maxClimbRate;
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@@ -178,6 +178,10 @@ public:
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_indicated_airspeed_max = airspeed;
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}
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void set_heightrate_p(float heightrate_p) {
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_heightrate_p = heightrate_p;
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}
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private:
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// Last time update_50Hz was called
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uint64_t _update_50hz_last_usec;
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@@ -201,6 +205,7 @@ private:
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float _vertAccLim;
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float _rollComp;
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float _spdWeight;
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float _heightrate_p;
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// throttle demand in the range from 0.0 to 1.0
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float _throttle_dem;
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