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| محاكاة الأجسام المتعددة (N-Body Simulation)× | مشكلة لامبرت (Lambert's problem)× | |
|---|---|---|
| المجال | الفيزياء التطبيقية | الفيزياء التطبيقية |
| العائلة | Process / pipeline | Process / pipeline |
| سنة النشأة≠ | 1687 | 1761 |
| صاحب الطريقة≠ | Isaac Newton | Johann Heinrich Lambert |
| النوع≠ | Computational simulation algorithm | Orbital computation algorithm |
| المصدر التأسيسي≠ | Poincaré, H. (1892). Les méthodes nouvelles de la mécanique céleste. Gauthier-Villars. link ↗ | Lambert, J. H. (1761). Acta Helvetica. Physico-Mathematico-Anatomico-Botanico-Medica. link ↗ |
| الأسماء البديلة | gravitational N-body problem, many-body simulation | Lambert's problem, Lambert-Godstein trajectory problem |
| ذات صلة≠ | 5 | 4 |
| الملخص≠ | N-body simulation is a computational method for modeling the dynamics of a system of particles under mutual gravitational forces. Originating from Newton's laws of motion and gravitation, it solves the fundamental equations of celestial mechanics. This technique is essential for understanding planetary orbits, star cluster evolution, and cosmological structure formation. | Lambert's problem is a classical astrodynamics boundary-value problem that determines an orbit connecting two points in space given a transfer time. Formulated by Johann Heinrich Lambert in the 18th century, it is fundamental to trajectory design for interplanetary missions and spacecraft maneuvers. The solution provides the orbital elements and velocities needed to transition between two positions. |
| ScholarGateمجموعة البيانات ↗ |
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