| Autor: |
Sokolsky, Andrej G., Vakhidov, Akmal A., Vasiliev, Nickolay N. |
| Zdroj: |
Celestial Mechanics and Dynamical Astronomy; September 1995, Vol. 63 Issue: 3-4 p357-374, 18p |
| Abstrakt: |
The problem of computation of elliptic Hansen coefficients and their derivatives is considered for constructing a motion theory of an artificial Earth satellite with large eccentricity. An algorithm for analytical and numerical computation of these coefficients and their derivatives is described. The recurrence relations for derivatives of the first and second order and initial values for recurrences are obtained. As an example, numerical values of some elliptic Hansen coefficients are given for the orbit with eccentricityk=0.74. |
| Databáze: |
Supplemental Index |
| Externí odkaz: |
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