Let "P(x, y)" be the position of the planet after time t after starting from rest from perihelion position A , referred to S as origin. Then
By Kepler's second law of motion, we have: the radius vector drawn from the centre of the sun to the planet sweeps out equal area in equal time. The rate of description of area is constant:
"{h\\over 2}={1 \\over 2}r^2 {d\\nu \\over dt}"
Hence
"{dx\\over dt}=-a\\sin\\theta{d\\theta\\over dt}, \\ {dy\\over dt}=b\\cos\\theta{d\\theta\\over dt}"
"h=(a\\cos \\theta-ae)b\\cos\\theta{d\\theta\\over dt}+b\\sin \\theta (a\\sin\\theta{d\\theta\\over dt})"
"h=ab(\\cos^2\\theta+\\sin^2\\theta-e\\cos\\theta){d\\theta\\over dt}"
"h=ab(1-e\\cos\\theta){d\\theta\\over dt}"
"hdt=ab(1-e\\cos\\theta)d\\theta"
Integrate
Initially when "t=0," the planet is is at A whose eccentric angle "\\theta=0."
Find "c_1"
Therefore
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