Changeset 17094 for trunk/HeuristicLab.Problems.Instances.DataAnalysis/3.3/Regression/Physics/AircraftLift.cs
- Timestamp:
- 07/05/19 18:15:56 (5 years ago)
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- 1 edited
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trunk/HeuristicLab.Problems.Instances.DataAnalysis/3.3/Regression/Physics/AircraftLift.cs
r17092 r17094 36 36 "modeling generalized separable systems\", Expert Systems with Applications, Volume 109, 2018, " + 37 37 "Pages 25-34 https://doi.org/10.1016/j.eswa.2018.05.021. " + Environment.NewLine + 38 "Function: C_L = C_Lα (α -α0) + C_Lδ_e δ_e S_HT / S_ref" + Environment.NewLine +38 "Function: C_L = C_Lα (α + α0) + C_Lδ_e δ_e S_HT / S_ref" + Environment.NewLine + 39 39 "the lift coefficient of the main airfoil C_Lα ∈ [0.4, 0.8]," + Environment.NewLine + 40 40 "tha angle of attack α ∈ [5°, 10°]," + Environment.NewLine + … … 48 48 49 49 protected override string TargetVariable { get { return "C_L"; } } 50 protected override string[] VariableNames { get { return new string[] { "C_Lα", "α", " α0", "C_Lδ_e", "δ_e", "S_HT", "C_L", "C_L_noise" }; } }51 protected override string[] AllowedInputVariables { get { return new string[] { "C_Lα", "α", " α0", "C_Lδ_e", "δ_e", "S_HT" }; } }50 protected override string[] VariableNames { get { return new string[] { "C_Lα", "α", "C_Lδ_e", "δ_e", "S_HT", "S_ref", "C_L", "C_L_noise" }; } } 51 protected override string[] AllowedInputVariables { get { return new string[] { "C_Lα", "α", "C_Lδ_e", "δ_e", "S_HT", "S_ref" }; } } 52 52 protected override int TrainingPartitionStart { get { return 0; } } 53 53 protected override int TrainingPartitionEnd { get { return 100; } }
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