Difference between revisions of "Orbital Dynamics"
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'''The motion of one body about another body due to gravity, is known as an Orbit. [[Orbits]] are described by a body of theory called "[[Orbital Dynamics]]". [[Kepler]] discovered that in [[Newtonian]] [[Physics]], which ignore [[Einstein]]'s theories of [[relativity]], orbits are [[elliptical]] in shape, at least for the simple case of one body orbiting another body without any influence from any third body. [[Kepler's Laws]] are three [[equations]] which describe elliptical orbits, and still hold true today.''' | '''The motion of one body about another body due to gravity, is known as an Orbit. [[Orbits]] are described by a body of theory called "[[Orbital Dynamics]]". [[Kepler]] discovered that in [[Newtonian]] [[Physics]], which ignore [[Einstein]]'s theories of [[relativity]], orbits are [[elliptical]] in shape, at least for the simple case of one body orbiting another body without any influence from any third body. [[Kepler's Laws]] are three [[equations]] which describe elliptical orbits, and still hold true today.''' | ||
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The force exerted by two bodies on each other is given by | The force exerted by two bodies on each other is given by | ||
Revision as of 06:59, 8 March 2007
Orbital dynamics is the study of the motion of objects in the presence of gravitational forces of other bodies. All bodies provide a gravitational pull on other bodies surrounding it.
The motion of one body about another body due to gravity, is known as an Orbit. Orbits are described by a body of theory called "Orbital Dynamics". Kepler discovered that in Newtonian Physics, which ignore Einstein's theories of relativity, orbits are elliptical in shape, at least for the simple case of one body orbiting another body without any influence from any third body. Kepler's Laws are three equations which describe elliptical orbits, and still hold true today.
Newton's Law of Gravity
The force exerted by two bodies on each other is given by
<math>F = \frac{Gm_{1}m_{2}}{r^{2}}</math>
where G is the Universal Gravitational Constant whose value is 6.67300 × 10-11 m3 kg-1 s-2, <math>m_1</math> is the mass of the first body, <math>m_2</math> is the mass of the second body, and r is the distance between them.
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