Changeset 17094


Ignore:
Timestamp:
07/05/19 18:15:56 (2 weeks ago)
Author:
gkronber
Message:

#3014: fixed bugs in AircraftLift problem description

File:
1 edited

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  • trunk/HeuristicLab.Problems.Instances.DataAnalysis/3.3/Regression/Physics/AircraftLift.cs

    r17092 r17094  
    3636          "modeling generalized separable systems\", Expert Systems with Applications, Volume 109, 2018, " +
    3737          "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 +
    3939          "the lift coefficient of the main airfoil C_Lα ∈ [0.4, 0.8]," + Environment.NewLine +
    4040          "tha angle of attack α ∈ [5°, 10°]," + Environment.NewLine +
     
    4848
    4949    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" }; } }
    5252    protected override int TrainingPartitionStart { get { return 0; } }
    5353    protected override int TrainingPartitionEnd { get { return 100; } }
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