The difference between an orbit and a revolution is explained and it is shown why space shuttle Columbia's period of revolution was longer than its orbital period. Parameters of orbits examined include apoapsis, periapsis, apogee, perigee, aphelion, perihelion, orbital plane, and inclination. Orbit velocity and duration, Newton's law of gravitation, and Kepler's three laws of motion are considered. The principles involved in geostationary satellites are also explored
The author's previous theory of the artificial satellite is derived in terms of the. disturbed eccen...
Current space exploration programs call for the establishment of a permanent Human presence on the M...
This article reports an investigation of the effect of solar radiation pressure on the motion of an ...
Fifty years after Sputnik, artificial satellites have become indispensable monitors in many areas, s...
<p>An orbit is the gravitationally curved path of an object about a point in space (Wikipedia). Sate...
Materials presented here outline some basic concepts associated with space flight. Users can read ab...
Application of celestial mechanics to artificial satellite orbit calculations using orbit perturbati...
Comparison of theoretical and measured orbital perturbations of artificial earth satellite
Abstract: In any system of bodies, relativistic considerations can provide only those parameters of ...
This discussion of orbits around the Earth and Sun begins by describing synchronous orbits and then ...
This book deals with the motion of the center of mass of a spacecraft; this discipline is generally ...
This book deals with the motion of the center of mass of a spacecraft; this discipline is generally ...
The relative motion problem is analyzed, as a linearized case, and as a numerically determined solut...
The problem of the two-body gravitational interaction has been solved numerically based on the class...
This chapter discusses fundamentals of orbital dynamics and provides a description of key perturbat...
The author's previous theory of the artificial satellite is derived in terms of the. disturbed eccen...
Current space exploration programs call for the establishment of a permanent Human presence on the M...
This article reports an investigation of the effect of solar radiation pressure on the motion of an ...
Fifty years after Sputnik, artificial satellites have become indispensable monitors in many areas, s...
<p>An orbit is the gravitationally curved path of an object about a point in space (Wikipedia). Sate...
Materials presented here outline some basic concepts associated with space flight. Users can read ab...
Application of celestial mechanics to artificial satellite orbit calculations using orbit perturbati...
Comparison of theoretical and measured orbital perturbations of artificial earth satellite
Abstract: In any system of bodies, relativistic considerations can provide only those parameters of ...
This discussion of orbits around the Earth and Sun begins by describing synchronous orbits and then ...
This book deals with the motion of the center of mass of a spacecraft; this discipline is generally ...
This book deals with the motion of the center of mass of a spacecraft; this discipline is generally ...
The relative motion problem is analyzed, as a linearized case, and as a numerically determined solut...
The problem of the two-body gravitational interaction has been solved numerically based on the class...
This chapter discusses fundamentals of orbital dynamics and provides a description of key perturbat...
The author's previous theory of the artificial satellite is derived in terms of the. disturbed eccen...
Current space exploration programs call for the establishment of a permanent Human presence on the M...
This article reports an investigation of the effect of solar radiation pressure on the motion of an ...