Mathematical Problems in Engineering

Mathematical Methods Applied to the Celestial Mechanics of Artificial Satellites 2013


Publishing date
28 Jun 2013
Status
Published
Submission deadline
08 Feb 2013

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 2013

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 possible live communications, exploration of Earth resources, weather forecast, accurate positioning, and several other tasks that are part of our lives today.

Therefore, since celestial mechanics plays a very important role in these developments, this call for papers is posted seeking for 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/mmac13/ according to the following timetable:


Articles

  • Special Issue
  • - Volume 2013
  • - Article ID 483457
  • - Research Article

Averaging Methods for Design of Spacecraft Hysteresis Damper

Ricardo Gama | Anna D. Guerman | ... | Georgi V. Smirnov
  • Special Issue
  • - Volume 2013
  • - Article ID 249674
  • - Research Article

Estimating Friction Parameters in Reaction Wheels for Attitude Control

Valdemir Carrara | Hélio Koiti Kuga
  • Special Issue
  • - Volume 2013
  • - Article ID 950675
  • - Research Article

A New Celestial Navigation Method for Spacecraft on a Gravity Assist Trajectory

Ning Xiaolin | Huang Panpan | Fang Jiancheng
  • Special Issue
  • - Volume 2013
  • - Article ID 745637
  • - Research Article

The Study of the Asymmetric Multiple Encounters Problem and Its Application to Obtain Jupiter Gravity Assisted Maneuvers

Denilson Paulo Souza dos Santos | Antônio Fernando Bertachini de Almeida Prado | Evandro Marconi Rocco
  • Special Issue
  • - Volume 2013
  • - Article ID 531672
  • - Research Article

Tangent Orbital Rendezvous Using Linear Relative Motion with Perturbations

Gang Zhang | Dongzhe Wang | ... | Zhaowei Sun
  • Special Issue
  • - Volume 2013
  • - Article ID 897579
  • - Research Article

Discrete Model Reference Adaptive Control for Gimbal Servosystem of Control Moment Gyro with Harmonic Drive

Bangcheng Han | Yanpeng Chen | ... | Lianhui Yang
  • Special Issue
  • - Volume 2013
  • - Article ID 570127
  • - Research Article

Averaging Tesseral Effects: Closed Form Relegation versus Expansions of Elliptic Motion

Martin Lara | Juan F. San-Juan | Luis M. López-Ochoa
  • Special Issue
  • - Volume 2013
  • - Article ID 601482
  • - Research Article

Circular Orbit Target Capture Using Space Tether-Net System

Guang Zhai | Jing-rui Zhang | Zhang Yao
  • Special Issue
  • - Volume 2013
  • - Article ID 191384
  • - Research Article

Precise Analytical Computation of Frozen-Eccentricity, Low Earth Orbits in a Tesseral Potential

Martin Lara | Juan F. San-Juan | Luis M. López-Ochoa
  • Special Issue
  • - Volume 2013
  • - Article ID 415015
  • - Research Article

Searching for Orbits with Minimum Fuel Consumption for Station-Keeping Maneuvers: An Application to Lunisolar Perturbations

Antonio Fernando Bertachini de Almeida Prado
Mathematical Problems in Engineering
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