Results 61 to 70 of about 1,847 (222)
The zonal satellite problem - I: Near-collision flow [PDF]
The force field described by a potential function of the form U = Σn k=1 ak/rk (r = distance between particles, ak = real parameters) models various concrete situations belonging to astronomy, physics, mechanics, astrodynamics, etc. The two-body
Mioc V., Stavinschi M.
doaj +1 more source
The evolution of lunar communication—From the beginning to the present
Since the beginning of the space age, the Moon has been the target of many missions from the 1950s to the present day. Radio communication plays a fundamental role in space vehicle projects because this is the most obvious way to communicate with the ground station and transmit control commands and scientific data.
Andrea Farkasvölgyi +2 more
wiley +1 more source
Applications of Parallel Processing to Astrodynamics [PDF]
AbstractParallel processing is being used to improve the catalog of earth orbiting satellites and for problems associated with the catalog. Initial efforts centered around using SIMD parallel processors to perform debris conjunction analysis and satellite dynamics studies.
S. Coffey, L. Healy, H. Neal
openaire +1 more source
A Design Method for Redundant Microthruster Layout With Allocation Error
The microthruster is generally chosen as the actuator of the drag‐free satellite control system, and the layout directly affects the stability of the satellite control. Due to the extremely rigorous objectives of drag‐free control, a design method for the redundant thruster layout is proposed in this paper to improve the control stability of the ...
Mingwei Chen +6 more
wiley +1 more source
Celestial mechanics and astrodynamics /
"A selection of technical papers based mainly on the American Institute of Aeronautics and Astronautics Astrodynamics Conference held at New Haven, Connecticut, August 19-21, 1963.Includes ...
Szebehely, Victor Goyzo,1921-1997(viaf)44450236edt +1 more
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Optimal Gliding Trajectories for Descent on Mars
In this paper, optimal gliding trajectories are analyzed, formulating an optimal control problem to be solved computationally via nonlinear programming.
Jhonathan Murcia-Piñeros +3 more
doaj +1 more source
This paper aims to investigate the effects of asteroid size and shape and solar radiation pressure in the trajectories of a spacecraft in transfers between the collinear equilibrium points of a binary non-spherical asteroid system.
L. B. T. Santos +3 more
doaj +1 more source
GENERAL CONCEPTS ABOUT SOLID BODY ASTRODYNAMICS
The paper presents the theoretical foundation of the dynamics of the solid body in gravitational movement in the outer space. It is known that the movement of solid bodies in space is subjects both the laws of Newton's classical mechanics and those of ...
Viorel Mihai Nani, Alin Nani
doaj
Aero-astrodynamics research review
Aero-astrodynamics research review, and report bibliography, July 1967 to August ...
Murphree, W. D.
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