Figure 3 depicts a situation with three reference frames: a stationary unprimed frame
, a moving primed frame
and a third, double primed frame
of an object that moves relative to both other frames,
and
. Each frame has dimensional axes rotated relative to the other frames as a result of the relative motion.
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When
,
, and
are parallel, the classical relation between them is:
| (18) |
Like Eq. (18), Eq. (19) still limits the speeds as measured by both observers to the maximum of
, which is also clear by inspection of the Figure. Some remarks will be made now on the probability of either of the equations to be the right one:
With
and
nearing
, the resulting
will also near
, which is in accordance with the classical view.
But if (as a matter of mathematical experiment) the range of
and
is extended beyond the maximum value of
then the plot looks like depicted in Fig. 5.
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The part from Fig. 4 can still be recognized but it is clear now that this actually forms part of a continuous function that extends beyond
. The part beyond
may not be used, solely because the classical function is not defined, nor ever shown to be valid, for such superluminal extensions (actually the space-like quadrants in the classical light cone). This fact strongly suggests that the graph from Fig. 4 is an approximation of the real function.
Finally, both Eqs. (18) and (19) are plotted together in Fig. 6.
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Equation (19) is almost identical for speeds below about
but begins to deviate at higher speeds. The top of Eq. (19) corresponds to
. From the circle diagram in Fig. 3 it shows that the time-speed of the object, as measured from frame
, then becomes zero. Equation (19) further shows decreasing values for
in situations where the values of
and
go beyond
(the frame of the moving object then rotates beyond
relative to frame
). It turns out that in that case the corresponding time-speed for the object becomes negative. (This situation might be related to anti-particles, running 'backwards in time'.).
The situation where
equals
gives the maximum possible deviation relative to the classical graph. Other ratios between
and
give (much) smaller deviations and the tops of Eq. (19) will shift outwards towards
as can be seen in Fig. 7 where the ratio between
and
equals 3:1. At a ratio 10:1 both plots are practically identical. Virtually all practical situations that require the velocity addition formula to be used exist under such circumstances, which indicates that a deviation from the classical graph is likely to remain unnoticed.
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The vast majority of experimental set-ups that are aimed at verification of relativity theory are using two reference frames. These experiments are not suitable for the verification of the velocity addition formula. One would have to use a set-up with three reference frames. At speeds on the order of
m/s the difference in resulting values between Eqs. (18) and (19) is on the order of
m/s, which might be noticeable using adequately accurate measuring devices.
A hypothetical case will now be used to show that Eq. (19) does not necessarily lead to causality conflicts as a result of the negative time-speeds that can occur.
A spaceship travels relative to Earth at speed
and heads toward an asteroid that is at rest relative to Earth. The ship launches a missile at the asteroid at
relative to the ship. An observer on the ship watches the missile destroy the asteroid. According to Eq. (19), an observer on Earth would see the missile traveling at only
so the missile's spatial speed is lower than that of the spaceship. It seems therefor that this observer would see the ship hit the asteroid before the missile.
The explanation of this paradox can be found in the comparison of the proper times of all objects involved. We call the proper time for the spaceship
and for the missile
.
For simplicity we set the space-time event of the launch at
and the distance between the spaceship and the asteroid at that moment at
light second (as measured by the observer on Earth).
The observer on Earth calculates time-coordinates of the impact (against the asteroid) using his own time
for the spaceship:
s; and for the missile:
s, so it seems as if the spaceship reaches the asteroid first. In 4D Euclidean space-time however the observer measures the time-speed
of the spaceship as:
.
According to this observer the absolute value of the timespeed
of the missile is
, but from the circle diagram (Fig. 3) it shows that we must now take the negative root so its value is
. Note that the cyclic nature of
now also implies that in this situation
has a negative value in
for the missile.
We calculate the proper times at the moment of impact according to the observer on Earth for the spaceship:
s; and for the missile:
s.
In proper time the missile hits the asteroid before the spaceship does despite its lower spatial speed. Causality is therefor not violated. The missile runs backwards in proper time.