37 lines
817 B
Matlab
37 lines
817 B
Matlab
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function dtr = sv_clock_bias(t, toc, a0, a1, a2, e, sqrtA, toe, Delta_n, M0)
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% 输入:
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% a0 a1 a2 toc: 卫星时钟校正模型方程中3个参数， toc: 第一数据块参考时间, 被用作时钟校正模型中时间参考点
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% dtr： 卫星时钟偏差
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dtr = a0+a1*(t-toc)+a2*(t-toc).^2;%t为未做钟差改正的观测时刻
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F = -4.442807633e-10;
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mu = 3.986005e14;
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A = sqrtA^2;
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cmm = sqrt(mu/A^3); % computed mean motion
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tk = t - toe;
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% account for beginning or end of week crossover
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if (tk > 302400)
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tk = tk-604800;
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end
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if (tk < -302400)
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tk = tk+604800;
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end
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% apply mean motion correction
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n = cmm + Delta_n;
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% Mean anomaly
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mk = M0 + n*tk;
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% solve for eccentric anomaly
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Ek = mk;
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Ek = mk + e*sin(Ek);
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Ek = mk + e*sin(Ek);
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Ek = mk + e*sin(Ek);
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% dsv 时间为s
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dtr = dtr + F*e*sqrtA*sin(Ek);
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end
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