Spacetime position paravector In the APS, the
spacetime position is represented as the paravector x = x^\mu\mathbf{e}_\mu = x^0 + x^1 \mathbf{e}_1 + x^2 \mathbf{e}_2 + x^3 \mathbf{e}_3, where the time is given by the scalar part ,
e0=1, and {
e1,
e2,
e3} is the standard
orthonormal basis for position space. Throughout the remainder of this article and unless stated otherwise, units such that are used, called
natural units. In the
Pauli matrix representation, the unit basis vectors are replaced by the Pauli matrices and the scalar part by the identity matrix. This means that the Pauli matrix representation of the space-time position is x \rightarrow \begin{pmatrix} x^0 + x^3 && x^1 - ix^2 \\ x^1 + ix^2 && x^0-x^3\end{pmatrix}
Lorentz transformations and rotors The restricted Lorentz transformations that preserve the direction of time and include rotations and boosts can be performed by an exponentiation of the spacetime rotation
biparavector W L = e^{W/2} . In the matrix representation, the Lorentz rotor is seen to form an instance of the group (
special linear group of degree 2 over the
complex numbers), which is the double cover of the
Lorentz group. The unimodularity of the Lorentz rotor is translated in the following condition in terms of the product of the Lorentz rotor with its Clifford conjugation \Lambda\widetilde{\Lambda} = \widetilde{\Lambda} \Lambda = 1 . This Lorentz rotor can be always decomposed in two factors, one
Hermitian (a
Lorentz boost), and the other
unitary (a 3-dimensional
rotation), such that \Lambda = L R . The unitary element
R is called a
rotor because this encodes rotations, and the Hermitian element
L encodes
boosts. The total object \Lambda is called a
Lorentz rotor.
Four-velocity paravector The
four-velocity (also
proper velocity or
spacetime velocity) is defined as the
derivative of the spacetime position paravector with respect to
proper time τ: u = \frac{d x }{d \tau} = \frac{d x^0}{d\tau} + \frac{d}{d\tau}(x^1 \mathbf{e}_1 + x^2 \mathbf{e}_2 + x^3 \mathbf{e}_3) = \frac{d x^0}{d\tau}\left[1 + \frac{d}{d x^0}(x^1 \mathbf{e}_1 + x^2 \mathbf{e}_2 + x^3 \mathbf{e}_3)\right]. This expression can be brought to a more compact form by defining the ordinary velocity as \mathbf{v} = \frac{d}{d x^0}(x^1 \mathbf{e}_1 + x^2 \mathbf{e}_2 + x^3 \mathbf{e}_3) , and recalling the definition of the
gamma factor: \gamma(\mathbf{v}) = \frac{1}{\sqrt{1-\frac{|\mathbf{v}|^2}{c^2}}} , so that the proper velocity is more compactly: u = \gamma(\mathbf{v})(1 + \mathbf{v}). The proper velocity is a positive
unimodular paravector, which implies the following condition in terms of the
Clifford conjugation u \widetilde{u} = 1 . The proper velocity transforms under the action of the Lorentz rotor \Lambda as u \rightarrow u^\prime = \Lambda u \Lambda^\dagger. This transformation law can be easily derived from the isomorphism between the APS and the even subalgebra of the STA.
Four-momentum paravector The
four-momentum (also
spacetime momentum) in the APS can be obtained by multiplying the proper velocity with the mass as p = m u, with the
mass shell condition translated into \widetilde{p}p = p\widetilde{p} = pp^-= p^-p= m^2 . The proper velocity
u may be represented as the Lorentz transformation of the rest velocity 1: u = \Lambda\Lambda^\dagger. This implies that the spacetime momentum can likewise be written as the Lorentz transformation of the rest momentum
m, p = \Lambda m\Lambda^\dagger. This trivial rewrite also connects the APS to other areas of
Physics; namely
helicity-spinor methods for
scattering amplitudes and for the
Constructive Standard Model (CSM). == Classical electrodynamics ==