Salīdzināt metodes

	Hohmanna pāreja	N-ķermeņu simulācija
Nozare	Lietišķā fizika	Lietišķā fizika
Saime	Process / pipeline	Process / pipeline
Izcelsmes gads	1925	1687
Autors	Walter Hohmann	Isaac Newton
Tips	Trajectory optimization algorithm	Computational simulation algorithm
Pirmavots	Hohmann, W. (1925). Die Erreichbarkeit der Himmelskörper. R. Oldenbourg.	Poincaré, H. (1892). Les méthodes nouvelles de la mécanique céleste. Gauthier-Villars.
Citi nosaukumi	Hohmann-Vallado transfer, two-impulse maneuver	gravitational N-body problem, many-body simulation
Saistītās	4	5
Kopsavilkums	The Hohmann transfer is a maneuver that transfers a spacecraft between two circular orbits using two impulsive burns (velocity changes). Introduced by German engineer Walter Hohmann in 1925, it is the most fuel-efficient method for coplanar orbital transfers when the transfer time is not severely constrained. The transfer orbit is an ellipse tangent to both the initial and final orbits.	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.