Last Updated：2025/11/26
When solving ordinary differential equations numerically for the orbital model, we used the Dormand-Prince method to obtain fourth- and fifth-order estimates with just six function evaluations and to use their difference as an error estimate.
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When solving ordinary differential equations numerically for the orbital model, we used the Dormand-Prince method to obtain fourth- and fifth-order estimates with just six function evaluations and to use their difference as an error estimate.
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軌道モデルの常微分方程式を数値的に解く際、6回の関数評価で4次と5次の解を算出し、その差を誤差推定として用いるドーマンド・プリンス法を使いました。
