About: Orbit modeling

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Orbit modeling is the process of creating mathematical models to simulate motion of a massive body as it moves in orbit around another massive body due to gravity. Other forces such as gravitational attraction from tertiary bodies, air resistance, solar pressure, or thrust from a propulsion system are typically modeled as secondary effects. Directly modeling an orbit can push the limits of machine precision due to the need to model small perturbations to very large orbits. Because of this, perturbation methods are often used to model the orbit in order to achieve better accuracy.

Attributes	Values
rdf:type	yago:WikicatOrbitalPerturbations yago:Abstraction100002137 yago:Agitation114403107 yago:Attribute100024264 yago:Condition113920835 yago:Disturbance114403282 yago:DynamicalSystem106246361 yago:PhaseSpace100029114 yago:PsychologicalState114373582 Election yago:Space100028651 yago:State100024720 yago:WikicatDynamicalSystems
rdfs:label	Modelizado de órbitas (es) Orbit modeling (en)
rdfs:comment	El modelizado de órbitas es el proceso de crear modelos matemáticos para simular el movimiento de un cuerpo masivo a medida que se mueve en órbita alrededor de otro cuerpo masivo debido a la gravedad. Otras fuerzas como la atracción gravitatoria de terceros cuerpos, la resistencia del aire, el viento solar o el empuje de un motor cohete, se suelen incluir en el modelo como efectos de segundo orden. Modelar directamente una órbita puede llevar a rebasar los límites de precisión de cálculo de los ordenadores, debido a la necesidad de modelar perturbaciones pequeñas en órbitas muy grandes. Debido a esto, los métodos de cálculo de perturbaciones a menudo se usan para modelar órbitas con el fin de lograr una mayor precisión. (es) Orbit modeling is the process of creating mathematical models to simulate motion of a massive body as it moves in orbit around another massive body due to gravity. Other forces such as gravitational attraction from tertiary bodies, air resistance, solar pressure, or thrust from a propulsion system are typically modeled as secondary effects. Directly modeling an orbit can push the limits of machine precision due to the need to model small perturbations to very large orbits. Because of this, perturbation methods are often used to model the orbit in order to achieve better accuracy. (en)
foaf:depiction
dct:subject	Dynamics of the Solar System Orbital perturbations Dynamical systems
Wikipage page ID	35539811 (xsd:integer)
Wikipage revision ID	1114608105 (xsd:integer)
Link from a Wikipage to another Wikipage	Perturbation (astronomy) Velocity Orbit Semi-major axis Sphere of influence (astrodynamics) Propulsion Conic section Conic sections Dynamics of the Solar System Mass Orbital perturbations Stumpff function Low Earth Orbit Equations of motion Geometry Gravimetry Gravitational constant Gravity Moon N-body problem Osculating orbit Long Duration Exposure Facility Machine precision Magnetic field Density Density of air Fundamental ephemeris True anomaly Three-body problem Two-body problem Drag coefficient Jet Propulsion Laboratory Development Ephemeris Acceleration Drag (physics) Euclidean vector Force Parameter Celestial mechanics Center of mass Significant figures Greenwich meridian Newton's law of universal gravitation Recurrence relation Isaac Newton Area Arithmetic Dynamical systems Kepler orbit Kilograms Sun Modeling and simulation Solar sail Newton's laws of motion Orbital eccentricity Orbital resonance Radiation pressure Solar wind Universal gravitational constant N-body simulation Standard gravitational parameter Thermosphere Position vector Periapsis Legendre polynomial Dimensionless number
Link from a Wikipage to an external page	http://www.fas.org/irp/imint/docs/rst/Intro/Part2_1b.html
sameAs	Orbit modeling Orbit modeling Orbit modeling Orbit modeling Orbit modeling
dbp:wikiPageUsesTemplate	dbt:Main dbt:NumBlk dbt:Reflist

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