Lagrange’s planetary equations

E157396

Lagrange’s planetary equations are a set of differential equations in celestial mechanics that describe how the orbital elements of a body evolve over time under perturbing forces.

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Predicate Object
instanceOf mathematical formulation in celestial mechanics
perturbation theory tool
set of differential equations
appliesTo two-body orbits with perturbations
assumes Keplerian reference orbit plus small perturbations
basedOn Lagrange’s variation of parameters method
canBeWrittenIn Gauss’s planetary equations
surface form: Gauss’s form of planetary equations

vectorial form
describes effects of perturbing forces on orbits
time evolution of orbital elements
domain classical mechanics
dynamical systems
expressedInTermsOf argument of periapsis
eccentricity
inclination
longitude of ascending node
mean anomaly or mean longitude
semi-major axis
field astrodynamics
celestial mechanics
orbital mechanics
goal predict long-term stability and evolution of orbits
historicalPeriod 18th century
influenced analytical theories of planetary motion
modern orbit determination methods
languageOfOriginalFormulation French
mathematicalNature first-order ordinary differential equations
namedAfter Joseph-Louis Lagrange
relatedTo Delaunay variables
Hamiltonian perturbation theory
canonical perturbation theory
relates perturbing accelerations to rates of change of orbital elements
requires perturbing potential or perturbing acceleration model
usedFor analysis of periodic orbital variations
analysis of secular orbital changes
long-term orbit propagation
mission design in astrodynamics
study of atmospheric drag effects
study of non-spherical gravity effects
study of planetary perturbations
study of radiation pressure effects
study of third-body perturbations
uses osculating orbital elements

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Gauss’s planetary equations relatedTo Lagrange’s planetary equations