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In [[astrodynamics]], A '''canonical unit''' is a [[unit of measurement]] defined in terms of an object's reference [[orbit]]. In this system, a reference mass, for example the sun, is assumed to be 1 "mass unit" and the mean distance from the orbiting object to the reference object is considered the "distance unit". | |||
Canonical units are useful when the precise distances and masses of objects in space are not available. However, by setting the mass of a given object to be 1 mass unit and the mean distance of the reference object to another object in question, many calculations can be simplified. | |||
== Overview == | |||
The ''Distance Unit'' <math>DU \ </math> is defined to be the mean radius of the reference orbit. | |||
The ''Time Unit'' <math>TU \ </math> is defined by the [[gravitational parameter]] <math> \mu\ </math>: | |||
<math>\mu = G*M\,\!</math> | |||
* <math>G \ </math> is the [[gravitational constant]] | |||
* <math>M \ </math> is the mass of the central reference body | |||
For canonical units, the gravitational parameter is defined as: | |||
<math>\mu = 1 * \frac{DU^3}{TU^2}</math> | |||
---- | |||
The quantity of the time unit (TU) can be solved in another unit system (e.g. the metric system) if the mass and radius of the central body has been determined. Using the above equation and applying [[dimensional analysis]], set the two equations expressing <math>\mu</math> equal to each other: | |||
<math>\mu = G*M = 1 * \frac{DU^3}{TU^2}</math> | |||
The time unit (TU) can be converted to another unit system for a more useful qualitative solution using the following equation: | |||
<math> TU = \sqrt{\frac{DU^3}{G*M}}</math> | |||
For Earth satellites, approximate unit conversions are as follows: | |||
* 1 DU = 6378.1 km = 20,925,524.97 ft | |||
* 1 DU/TU = 7.90538 km/s = 25,936.29 ft/sec | |||
* 1 TU = 806.80415 s | |||
== Astronomical Unit == | |||
The [[astronomical unit]] is a canonical unit based on the orbit of the Earth around the Sun | |||
== See also == | |||
*[[Astronomical unit]] | |||
*[[Conversion of units]] | |||
== References == | |||
Roger R. Bate, Donald D. Mueller, Jerry E. White. ''Fundamentals of Astrodynamics''. | |||
[[Category:Astrodynamics]] | |||
[[Category:Celestial mechanics]] |
Revision as of 00:02, 17 January 2014
In astrodynamics, A canonical unit is a unit of measurement defined in terms of an object's reference orbit. In this system, a reference mass, for example the sun, is assumed to be 1 "mass unit" and the mean distance from the orbiting object to the reference object is considered the "distance unit".
Canonical units are useful when the precise distances and masses of objects in space are not available. However, by setting the mass of a given object to be 1 mass unit and the mean distance of the reference object to another object in question, many calculations can be simplified.
Overview
The Distance Unit is defined to be the mean radius of the reference orbit.
The Time Unit is defined by the gravitational parameter :
- is the gravitational constant
- is the mass of the central reference body
For canonical units, the gravitational parameter is defined as:
The quantity of the time unit (TU) can be solved in another unit system (e.g. the metric system) if the mass and radius of the central body has been determined. Using the above equation and applying dimensional analysis, set the two equations expressing equal to each other:
The time unit (TU) can be converted to another unit system for a more useful qualitative solution using the following equation:
For Earth satellites, approximate unit conversions are as follows:
- 1 DU = 6378.1 km = 20,925,524.97 ft
- 1 DU/TU = 7.90538 km/s = 25,936.29 ft/sec
- 1 TU = 806.80415 s
Astronomical Unit
The astronomical unit is a canonical unit based on the orbit of the Earth around the Sun
See also
References
Roger R. Bate, Donald D. Mueller, Jerry E. White. Fundamentals of Astrodynamics.