Special Relativity Simulation of Mars



Relativity and the orbit of Mars

The orbit of Mars in the algorithm orbit-gravity-sim-12.exe firstly shows how the velocity adjustment from Special Relativity alters the orbit of Mars. The orbit of Mars here also demonstrates how the polygon error-margin occurs in Newtonian gravity (in conjunction with quantum time).

I am suggesting that because this orbit almost fits exactly into an equal number of sides in the orbit-polygon, a process occurs by which the data reveals that for 14 orbits, the orbit becomes increasingly eccentric, and then turns around and becomes more circular for 28 orbits. Theoretically the orbit should oscillate like this indefinitely, maintaining an average distance from the Sun throughout. (See Scenario [16] running at a time-ratio of 1:1 million).

So for the first 14 orbits, the maximum increases while the minimum decreases, after which they switch around. So after 28 orbits, they are almost back where they started. This is explained in more detail in Section 27 (Using OGS12). Here is some detail from Scenario [16]:

mars newton-orbit
Pay special attention to the parts highlighted in red, which represents the maximum distance from the Sun which Mars has fluctuated after the 28th orbit: about 67 meters. This is an average of just 2.5m per orbit over the 27 orbits. However, for the individual orbit #3 the distance from Mars to the Sun fluctuates by 380 meters. (Ignore the orbit #1 differences as they have no previous orbit to differ from, and just reflect the difference from the start).

Can you see how the orbit will become more eccentric due to the quantum nature of orbital polygons from orbit #1 to orbit #14? And then from orbit #15 onwards, they now become less eccentric. But the key concept is that this effect is simply a coincidental error caused by the computer algorithm. If the time-rate is changed so that the software generates an orbit with a different number of sides to the polygon, then the phenomenon simply disappears. If you want the full data of all the orbits, you can generate it in the software yourself.

Or see this link: www.flight-light-and-spin.com/simulator/mars-newton.txt

The next image shows detail of 28 orbits of Mars under Special Relativity. I have taken a similar orbit sample to the previous one. Scenario [17] follows:

mars special-relativity orbit
As can be seen, the orbit of Mars is also fairly eccentric so it reflects a significant adjustment due to Special Relativity. The total outward drift from the polygon error does not switch around at orbit#14 and orbit#15 like it does under Newton (Scenario [16]).

Instead by orbit #28, Mars is 18km closer to the Sun. This is about 2/3rd of a kilometre per orbit on average that Mars would be moving towards the Earth’s orbit – if the limit at the velocity of light from Special Relativity causes a decrease in expected velocity.

With Mars being 54 mkm away from the Earth, and the effect of Special Relativity on the orbit of the Earth being an inwards spiral of only about 100m per year, we can expect Mars to collide with the Earth in about 60 million years – but if and only if – Einstein’s theory of Special Relativity is correct. The effect of Special Relativity on the orbit of the Earth being about 100m per orbit is much less than it is on Mars because the Earth’s orbit is less eccentric than Mars’ orbit is.

Now in the previous chapter I highlighted several interpretations of how the Special Relativity’s limit on the velocity of light is calculated.

special relativity velocity formula
Special Relativity also claims that this loss in energy has to be compensated with an increase in the mass of the object – in order to preserve the conservation of energy principle. Moreover Feynman concludes that if the added velocity in the formula above ‘u’ is negative, then the formula is not reversible. So for him ‘u’ must be a positive number. No mass is lost or velocity gained if the object decreases away from light-speed.

On p.88 of Six Not-so-easy-pieces, Feynman discusses how two objects collide under the principles of Special Relativity:

Now Miles Mathis disagrees with Feynman on this point. For Mathis, ‘u’ can actually contain a negative number. This would mean that Mars will not be colliding with Earth in 60 million years time. Mathis’ evaluation of Special Relativity§ is wholly more acceptable – because the time-frames computed by OGS12 (using Feynman’s interpretation) are going to result in the Earth’s orbit being about 30 million kilometres further from the Sun 300 million years ago. If this were true then the dinosaurs would have been living in an extremely frigid ice-age.

So Mathis can not only ‘save’ the Earth from a horrible collision with Mars, but he could also save some face for the Relativists. It is vital to see that Mathis’ interpretation is not the standard one. Note how the standard concept specifically considers an ‘approach’ to the velocity of light, and not a decrease away from the velocity of light.

§ www.milesmathis.com/rel4.html

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This is an extract summary of Chapter XXX of the book: Flight Light and Spin
Download page for relativity simulation: algorithm orbit-gravity-sim-12.exe

The full chapter can be downloaded here: Sum-Theory.pdf
(5.5 mb, 57 pages, this pdf file is too big for chrome, use firefox)

List of: abbreviated short articles

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Relativity simulator