scientific article; zbMATH DE number 3802858

zbMath0508.70009MaRDI QIDQ4747620

V. A. Brumberg

Publication date: 1980

Title: zbMATH Open Web Interface contents unavailable due to conflicting licenses.

zbMATH Keywords

satellitefast and slow variablesplanetalgorithmization of analytic celectial mechanicsanalytic and semi- analytic methodscomputerized formulationexpansion of perturbation function and right-hand sides of equations of motionshort-term theories

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Astronomy and astrophysics (85A99) Celestial mechanics (70F15) Research exposition (monographs, survey articles) pertaining to mechanics of particles and systems (70-02) Software, source code, etc. for problems pertaining to mechanics of particles and systems (70-04)

Related Items (17)

General planetary theory in elliptic functions ⋮ Derivation of evolutionary equations in the many-body problem with isotropically varying masses using computer algebra ⋮ Hamiltonian formalism for Euler parameters ⋮ Quaternion methods and models of regular celestial mechanics and astrodynamics ⋮ Quaternion methods and regular models of celestial mechanics and space flight mechanics: the use of Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. I: Review and analysis of methods and models and their applications ⋮ Quaternion methods and regular models of celestial and space flight mechanic: using Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. II: Perturbed spatial restricted three-body problem ⋮ Investigation of the restricted problem of three bodies of variable masses using computer algebra ⋮ Applications of computer algebra in the study of the two-planet problem of three bodies with variable masses ⋮ Inertial navigation in space using the regular quaternion equations of astrodynamics ⋮ Perturbed spatial two-body problem: regular quaternion equations of relative motion ⋮ On the use of quaternions and Euler-Rodrigues symmetric parameters with moments and moment potentials ⋮ Analysis of optimal motion control for a material point in a central field with application of quaternions ⋮ Symbolic calculations in studying the problem of three bodies with variable masses ⋮ Optimal rotation of the orbit plane of a variable mass spacecraft in the central gravitational field by means of orthogonal thrust ⋮ Expansions of elliptic motion based on elliptic function theory ⋮ Global regularization of the orbits of relative motion in a version of the many-body problem ⋮ New approach to determining planetary perturbations in lunar theory

This page was built for publication: