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Fix deprecation of operator << for matrices in Armadillo 10.1
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@ -27,15 +27,9 @@ const double STRP_PI = 3.1415926535898; // Pi as defined in IS-GPS-200K
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arma::mat Skew_symmetric(const arma::vec &a)
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arma::mat Skew_symmetric(const arma::vec &a)
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{
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{
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arma::mat A = arma::zeros(3, 3);
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arma::mat A = {{0.0, -a(2), a(1)},
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{a(2), 0.0, -a(0)},
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A << 0.0 << -a(2) << a(1) << arma::endr
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{-a(1), a(0), 0.0}};
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<< a(2) << 0.0 << -a(0) << arma::endr
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<< -a(1) << a(0) << 0 << arma::endr;
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// {{0, -a(2), a(1)},
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// {a(2), 0, -a(0)},
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// {-a(1), a(0), 0}};
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return A;
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return A;
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}
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}
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@ -383,14 +377,11 @@ void ECEF_to_Geo(const arma::vec &r_eb_e, const arma::vec &v_eb_e, const arma::m
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double sin_lat = sin(LLH(0));
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double sin_lat = sin(LLH(0));
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double cos_long = cos(LLH(1));
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double cos_long = cos(LLH(1));
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double sin_long = sin(LLH(1));
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double sin_long = sin(LLH(1));
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// C++11 and arma >= 5.2
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// arma::mat C_e_n = {{-sin_lat * cos_long, -sin_lat * sin_long, cos_lat},
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arma::mat C_e_n = {{-sin_lat * cos_long, -sin_lat * sin_long, cos_lat},
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// {-sin_long, cos_long, 0},
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{-sin_long, cos_long, 0},
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// {-cos_lat * cos_long, -cos_lat * sin_long, -sin_lat}}; //ECEF to Geo
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{-cos_lat * cos_long, -cos_lat * sin_long, -sin_lat}}; // ECEF to Geo
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arma::mat C_e_n = arma::zeros(3, 3);
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C_e_n << -sin_lat * cos_long << -sin_lat * sin_long << cos_lat << arma::endr
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<< -sin_long << cos_long << 0 << arma::endr
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<< -cos_lat * cos_long << -cos_lat * sin_long << -sin_lat << arma::endr; // ECEF to Geo
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// Transform velocity using (2.73)
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// Transform velocity using (2.73)
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v_eb_n = C_e_n * v_eb_e;
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v_eb_n = C_e_n * v_eb_e;
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@ -417,14 +408,9 @@ void Geo_to_ECEF(const arma::vec &LLH, const arma::vec &v_eb_n, const arma::mat
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((1 - e * e) * R_E + LLH(2)) * sin_lat};
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((1 - e * e) * R_E + LLH(2)) * sin_lat};
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// Calculate ECEF to Geo coordinate transformation matrix using (2.150)
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// Calculate ECEF to Geo coordinate transformation matrix using (2.150)
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// C++11 and arma>=5.2
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arma::mat C_e_n = {{-sin_lat * cos_long, -sin_lat * sin_long, cos_lat},
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// arma::mat C_e_n = {{-sin_lat * cos_long, -sin_lat * sin_long, cos_lat},
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{-sin_long, cos_long, 0},
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// {-sin_long, cos_long, 0},
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{-cos_lat * cos_long, -cos_lat * sin_long, -sin_lat}};
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// {-cos_lat * cos_long, -cos_lat * sin_long, -sin_lat}};
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arma::mat C_e_n = arma::zeros(3, 3);
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C_e_n << -sin_lat * cos_long << -sin_lat * sin_long << cos_lat << arma::endr
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<< -sin_long << cos_long << 0 << arma::endr
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<< -cos_lat * cos_long << -cos_lat * sin_long << -sin_lat << arma::endr;
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// Transform velocity using (2.73)
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// Transform velocity using (2.73)
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v_eb_e = C_e_n.t() * v_eb_n;
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v_eb_e = C_e_n.t() * v_eb_n;
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@ -453,10 +439,9 @@ void pv_Geo_to_ECEF(double L_b, double lambda_b, double h_b, const arma::vec &v_
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((1 - pow(e, 2)) * R_E + h_b) * sin_lat};
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((1 - pow(e, 2)) * R_E + h_b) * sin_lat};
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// Calculate ECEF to Geo coordinate transformation matrix using (2.150)
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// Calculate ECEF to Geo coordinate transformation matrix using (2.150)
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arma::mat C_e_n = arma::zeros(3, 3);
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arma::mat C_e_n = {{-sin_lat * cos_long, -sin_lat * sin_long, cos_lat},
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C_e_n << -sin_lat * cos_long << -sin_lat * sin_long << cos_lat << arma::endr
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{-sin_long, cos_long, 0.0},
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<< -sin_long << cos_long << 0 << arma::endr
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{-cos_lat * cos_long, -cos_lat * sin_long, -sin_lat}};
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<< -cos_lat * cos_long << -cos_lat * sin_long << -sin_lat << arma::endr;
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// Transform velocity using (2.73)
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// Transform velocity using (2.73)
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v_eb_e = C_e_n.t() * v_eb_n;
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v_eb_e = C_e_n.t() * v_eb_n;
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