(32SII) Tracing the Orbit Coordinates
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08-13-2017, 01:13 PM
Post: #1
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(32SII) Tracing the Orbit Coordinates
Link to the blog post: http://edspi31415.blogspot.com/2017/08/h...nates.html
The following program tracks the position (x,y) of a satellite in orbit by solving the pair of second-order differential equations: d^2 x/dt^2 = -α * x * (x^2 + y^2)^-1.5 d^2 y/dt^2 = -α * y * (x^2 + y^2)^-1.5 For planetary orbits, α = G * M Variables and Labels Labels Used: 4 (A, B, C, D) Variables Used: Pre stored variables: X = x0, initial x position U = dx/dt, velocity of x coordinate Y = y0, initial y position V = dy/dt, velocity of y coordinate C = Δt, desired time increment A = α, gravitational force factor If you are analyzing planetary orbits, then α = G * M where M is the mass of the center object and G is the Universal gravitational constant, G = 6.67384 * 10^-11 (m^3)/(s^2 * kg). Other: T = t This program is based off of the HP 25S and program authored Robert M. Eisberg. (see the source below) HP 32SII Program (87.5 bytes) Code:
Example Pre stored variables: X = 1.5 U = 0.18 Y = 1.5 V = 0.23 C = 1 A = α = 1 Table: T = X = Y = 0 (initial) 1.5 1.5 1 1.6014 1.6514 2 1.5713 1.6672 3 1.4105 1.5443 4 1.0956 1.2527 5 0.5429 0.6892 6 -0.8138 -0.8949 Source: Robert M. Eiseberg. Applied Mathematical Physics with Programmable Calculators McGraw Hill. 1976. ISBN 0-07-019109-3 |
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