Mathematical Problems in Engineering

Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites 2014


Publishing date
03 Oct 2014
Status
Published
Submission deadline
16 May 2014

1Instituto Nacional de Pesquisas Espaciais, 12227-010 São José dos Campos, SP, Brazil

2Departament de Matemática Aplicada I, Universitat Politécnica de Catalunya, 08028 Barcelona, Spain

3São Paulo State University Júlio de Mesquita Filho, FEG-UNESP, São Paulo, SP, Brazil

4Grupo Dinamica Orbital Planetologia, São Paulo State University Júlio de Mesquita Filho, São Paulo, SP, Brazil

5Departamento de Estatística, Matemática Aplicada e Computacão, São Paulo State University Júlio de Mesquita Filho, São Paulo, SP, Brazil


Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites 2014

Description

The idea of this special issue of mathematical problems in engineering is to consider the study and applications of celestial mechanics in artificial satellites. This science is very old in human history and deals with problems related to the motion of the planets, satellites, stars, and any celestial body that moves in space governed by the attraction of mass. Many important questions have been answered by this science, related to the motion of the Earth, Moon, and so forth. In the last decades, this science has also been applied to the motion of spacecraft made and launched by man into space. Some of the main tasks of this modern activity are to determine the orbit and the attitude of the spacecraft based on some observations, to obtain its position and attitude in space in a given time from some initial conditions, to find the best way to change their orbits and attitude, to analyze how to use the information of the satellites to find the position and the velocity of a given point (e.g., a personal receptor, a satellite, or a car), and so on.

Those applications show that the space activity in the world is one of the most important achievements of mankind. It makes live communications, exploration of Earth resources, weather forecast, accurate positioning, and several other tasks that are part of our lives today possible.

Therefore, since celestial mechanics plays a very important role in these developments, this call for papers is posted to seek papers related to the study of the engineering applications devoted to the motion of spacecrafts. Potential topics include, but are not limited to:

  • Astrodynamics
  • Orbital maneuver
  • Satellite dynamics and control
  • Aerospace engineering
  • Space dynamics
  • Dynamical systems

Before submission authors should carefully read over the journal's Author Guidelines, which are located at http://www.hindawi.com/journals/mpe/guidelines/. Prospective authors should submit an electronic copy of their complete manuscript through the journal Manuscript Tracking System at http://mts.hindawi.com/submit/journals/mpe/mmac14/ according to the following timetable:


Articles

  • Special Issue
  • - Volume 2015
  • - Article ID 940427
  • - Editorial

Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites 2014

Antonio F. Bertachini A. Prado | Josep J. Masdemont | ... | Vivian Martins Gomes
  • Special Issue
  • - Volume 2015
  • - Article ID 493903
  • - Research Article

Mapping Orbits regarding Perturbations due to the Gravitational Field of a Cube

Flaviane C. F. Venditti | Antonio F. B. A. Prado
  • Special Issue
  • - Volume 2014
  • - Article ID 854967
  • - Research Article

A Simple Time Domain Collocation Method to Precisely Search for the Periodic Orbits of Satellite Relative Motion

Xiaokui Yue | Xuechuan Wang | Honghua Dai
  • Special Issue
  • - Volume 2014
  • - Article ID 820586
  • - Research Article

Satellite Attitude Control System Design Taking into Account the Fuel Slosh and Flexible Dynamics

Alain G. de Souza | Luiz C. G. de Souza
  • Special Issue
  • - Volume 2014
  • - Article ID 302716
  • - Research Article

FDIR for the IMU Component of AOCS Systems

Maurício N. Pontuschka | Ijar M. da Fonseca
  • Special Issue
  • - Volume 2014
  • - Article ID 471352
  • - Research Article

Designing a Robust Nonlinear Dynamic Inversion Controller for Spacecraft Formation Flying

Inseok Yang | Dongik Lee | Dong Seog Han
  • Special Issue
  • - Volume 2014
  • - Article ID 927975
  • - Research Article

Numerical Validation of the Delaunay Normalization and the Krylov-Bogoliubov-Mitropolsky Method

David Ortigosa | Juan Félix San-Juan | ... | Montserrat San-Martín
  • Special Issue
  • - Volume 2014
  • - Article ID 508516
  • - Research Article

Guidance and Control of Position and Attitude for Rendezvous and Dock/Berthing with a Noncooperative/Target Spacecraft

Gilberto Arantes | Luiz S. Martins-Filho
  • Special Issue
  • - Volume 2014
  • - Article ID 359845
  • - Research Article

Effects of the Eccentricity of a Perturbing Third Body on the Orbital Correction Maneuvers of a Spacecraft

R. C. Domingos | A. F. B. A. Prado | V. M. Gomes
  • Special Issue
  • - Volume 2014
  • - Article ID 678015
  • - Research Article

Effects of Geopotential and Atmospheric Drag Effects on Frozen Orbits Using Nonsingular Variables

Paula Cristiane Pinto Mesquita Pardal | Rodolpho Vilhena de Moraes | Helio Koiti Kuga
Mathematical Problems in Engineering
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Acceptance rate11%
Submission to final decision118 days
Acceptance to publication28 days
CiteScore2.600
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