Using changing acceleration due to gravity?

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SUMMARY

The discussion focuses on the application of Newton's law of universal gravitation, expressed as ma = GmM/r^2, to derive accurate displacement equations under varying gravitational acceleration. The user seeks clarity on integrating acceleration equations, specifically questioning the validity of using a = c/(r-x)^2 for displacement calculations. Recommendations include studying advanced mechanics texts that cover planetary motion and the mathematical foundations necessary for understanding these concepts.

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  • Understanding of Newton's law of universal gravitation
  • Familiarity with calculus, particularly integration techniques
  • Knowledge of kinematics and dynamics in physics
  • Basic concepts of planetary motion and orbits
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  • Study advanced mechanics textbooks focusing on planetary motion
  • Learn integration techniques for differential equations in physics
  • Explore the derivation of displacement equations under variable acceleration
  • Research the mathematical modeling of gravitational forces in orbital mechanics
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Wooh
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We know that, with gravity for example, that ma = GmM/r^2. For simplicity's sake and the sake of my question, let us say that a=c/r^2, where c is GM. Basically, I am wondering how I can use this to create the most accurate displacement equations possible. My problem, however, is that a is dv/dt...or dx^2/dt^2, but I doubt you can do dx^2/r=cdt^2 and integrate twice or whatnot.

Does anyone have some clarity? I have though to do a=c/(r-x)^2, where r is the initial distance and x is the distance traveled, but that still yields nothing helpful.
 
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I recommend studying a good mechanics book that discusses planetary motion. Exactly those equations solved to find planetary orbits and the like. However, it's not for the faint of heart if you're just starting out!
 

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