| Revision as of 00:09, 4 April 2002 edit213.253.39.205 (talk) another subheading← Previous edit | Revision as of 00:10, 4 April 2002 edit undo213.253.39.205 (talk) fixups, again geosynch != geostat in generalNext edit → | ||
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| This can be demonstrated analytically by application of the ] and the physics of ]. Drawing the ] and using the analysis methods of ] and ] allows the determination of the distance from Earth's center of mass which will satisfy this specified operating condition. | This can be demonstrated analytically by application of the ] and the physics of ]. Drawing the ] and using the analysis methods of ] and ] allows the determination of the distance from Earth's center of mass which will satisfy this specified operating condition. | ||
| ''' |
'''Circular geosynchronous orbits''' | ||
| An ideal circular orbit that kept the satellite over a single point on the Earth's equator at all times is called a ]. | An ideal circular orbit that kept the satellite over a single point on the Earth's equator at all times is called a ]. | ||
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| :insert Tex or other math here | :insert Tex or other math here | ||
| '''Active |
'''Active geosynchronous orbits''' | ||
| Theoretically ] can use active thrust to balance a portion of the gravity forces experienced. Thus it can be "geo synchronous" in an orbit different from the traditional definition established in the early era of initial space exploration activities. | Theoretically ] can use active thrust to balance a portion of the gravity forces experienced. Thus it can be "geo synchronous" in an orbit different from the traditional definition established in the early era of initial space exploration activities. | ||
Revision as of 00:10, 4 April 2002
A geosynchronous orbit is an orbit that has the same rotational period and direction as the rotation of the Earth.
An object in a circular geosynchronous orbit in the plane of the Earth's equator would have a radius of approximately 42,164 km from the center of the Earth, approximately 35,787 km above mean sea level.
This can be demonstrated analytically by application of the Law of Gravity and the physics of centripetal acceleration. Drawing the free body diagram and using the analysis methods of engineering dynamics and Physics allows the determination of the distance from Earth's center of mass which will satisfy this specified operating condition.
Circular geosynchronous orbits
An ideal circular orbit that kept the satellite over a single point on the Earth's equator at all times is called a geostationary orbit.
In general, a perfect stable geostationary orbit is an ideal that can only be approximated. In practice, several different practical methods of station keeping allow satellites to remain over a required region of the Earth's surface.
The name Clarke Belt has been given to the a belt approximately 35,787 km directly above Earth's equator where near-geostationary orbits may be achieved. Science fiction writer and scientist Arthur C. Clarke wrote about this belt in 1945, hence the name. Clarke's vision of geostationary communications satellites was made a reality in 1962 with the launch of Telstar.
Elliptical geosynchronous orbits
Elliptical orbits can and are designed for communications satellites that keep the satellite within view of its assigned ground stations or recievers.
A satellite in an elliptical geosynchronous orbit will appear to oscillate in the sky from the viewpoint of a ground station, and satellites in highly elliptical orbits must be tracked by steerable ground stations.
Free Body Diagram
- insert diagram here
- insert Tex or other math here
Active geosynchronous orbits
Theoretically Statites can use active thrust to balance a portion of the gravity forces experienced. Thus it can be "geo synchronous" in an orbit different from the traditional definition established in the early era of initial space exploration activities.