Gravitational Force: Explaining -Fgrav*(x/r) to Tom Koolen

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SUMMARY

The discussion centers on the gravitational force acting on a satellite, specifically the equation -Fgrav*(x/r), where r represents the distance from the satellite to the Earth. Participants clarify that the gravitational force vector points towards the center of the Earth, and the x and y components can be computed using trigonometric functions, specifically the sine and cosine of the angle formed. A diagram illustrating the Cartesian axes and the radial vector is recommended for better understanding.

PREREQUISITES
  • Understanding of gravitational force and its mathematical representation
  • Knowledge of Cartesian coordinate systems
  • Familiarity with trigonometric functions, particularly sine and cosine
  • Basic physics concepts related to satellite motion
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  • Study the derivation of gravitational force equations in classical mechanics
  • Learn about vector decomposition in physics
  • Explore the concept of orbital mechanics and satellite dynamics
  • Review trigonometric identities and their applications in physics problems
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Students of physics, educators explaining gravitational concepts, and anyone interested in satellite dynamics and orbital mechanics.

tomkoolen
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Hello everyone,

We regard a satellite with only the gravitational force working on it.
My textbook states that the net force in the x-direction is: -Fgrav*(x/r), with r being the distance between the satellite and the Earth. Could anybody explain this to me?

Thanks in advance,
Tom Koolen
 
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Draw a diagram with the Cartesian axes centered on the Earth. The radial vector from the origin to the satellite has length r. Now look at the satellite. What direction does the gravitational force vector act? How might you compute its x and y components?
 
Oh yeah, of course it's the sine of that angle! Thanks :)
 

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