We want to express the coordinates and of an inertial frame in terms of the coordinates and of another inertial frame We will assume that the two frames meet the following conditions:
their spacetime coordinate origins coincide ( mark the same spacetime location as ),
their space axes are parallel, and
moves with a constant velocity relative to
What we know at this point is that whatever moves with a constant velocity in will do so in It follows that the transformation maps straight lines in onto straight lines in Coordinate lines of in particular, will be mapped onto straight lines in This tells us that the dashed coordinates are linear combinations of the undashed ones,
We also know that the transformation from to can only depend on so and are functions of Our task is to find these functions. The real-valued functions and actually can depend only on so and A vector function depending only on must be parallel (or antiparallel) to and its magnitude must be a function of We can therefore write and (It will become clear in a moment why the factor is included in the definition of ) So,
Let's set equal to This implies that As we are looking at the trajectory of an object at rest in must be constant. Hence,
Let's write down the inverse transformation. Since moves with velocity relative to it is
To make life easier for us, we now chose the space axes so that Then the above two (mutually inverse) transformations simplify to
Plugging the first transformation into the second, we obtain
The first of these equations tells us that
and
The second tells us that
and
Combining with (and taking into account that ), we obtain
Using to eliminate we obtain and
Since the first of the last two equations implies that we gather from the second that
tells us that must, in fact, be equal to 1, since we have assumed that the space axes of the two frames a parallel (rather than antiparallel).
With and yields Upon solving for we are left with expressions for and depending solely on :
Quite an improvement!
To find the remaining function we consider a third inertial frame which moves with velocity relative to Combining the transformation from to
with the transformation from to
we obtain the transformation from to :
The direct transformation from to must have the same form as the transformations from to and from to , namely
where is the speed of relative to Comparison of the coefficients marked with stars yields two expressions for which of course must be equal:
It follows that and this tells us that
is a universal constant. Solving the first equality for we obtain
This allows us to cast the transformation
into the form
Trumpets, please! We have managed to reduce five unknown functions to a single constant.