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A rotating spatial basis is not an inertial frame: nonzero coordinate acceleration of a uniform motion

Physical scope

A worked kinematic example of the framework: a uniformly rotating spatial basis field in a fixed inertial frame, and the coordinate acceleration of a worldline that is at rest in the inertial frame. The example verifies the rotating-frame acceleration identity of its mathematical supplier and shows that the rotating basis is not an inertial frame of the model. It asserts no force law, makes no claim about fictitious forces or measured effects, and contains no relativity content.

Example

Take the concrete model data of Adopted Newtonian spacetime structure: absolute time, Euclidean spatial slices and their smooth structure: V=R4 with coordinates (x0,x1,x2,x3), τ=x0, K={0}×R3 with the standard inner product g, A=R4 with its standard affine structure, the standard orientation; the first inertial frame F is the standard one, o=0, u=(1,0,0,0), ej the standard basis, with coordinates (t,x)=(t,x1,x2,x3), times in seconds and lengths in metres.

Let I=R and let ω>0 be a constant angular-speed parameter with [ω]=τ−1, read in s−1; radian angles are dimensionless by Dimensions and SI unit conventions of the non-relativistic classical mechanics framework, so ωs is dimensionless. In the displayed formulas s and ω denote their numerical values in seconds and inverse seconds. Define a time-dependent orthonormal basis field of K on I by

e~1(s)=cos⁡(ωs) e1+sin⁡(ωs) e2,e~2(s)=−sin⁡(ωs) e1+cos⁡(ωs) e2,e~3(s)=e3,

and the associated rotation matrix

R(s)=(cos⁡(ωs)−sin⁡(ωs)0sin⁡(ωs)cos⁡(ωs)0001),so that(e1,e2,e3) R(s)=(e~1(s),e~2(s),e~3(s)).

For a worldline that is at rest in F at the position (1 m,0,0), with F-coordinate curve x(s)=(1,0,0), define the rotating-basis coordinate curve y(s) by the expansion x(s)=R(s) y(s), that is, y(s):=R(s)Tx(s); the time coordinate is unchanged because the basis field rotates in K only.

Facts & Assumptions

Given: The model data and the frames and curves of the Example, with R:I→SO(3) the rotation matrix displayed above and ω>0; write x for the F-coordinate curve and y for the rotating-basis coordinate curve.

[L1]

The functions sin⁡ and cos⁡ are defined by their power series, are differentiable on R, with (sin⁡)′=cos⁡, (cos⁡)′=−sin⁡, and sin⁡0=0, cos⁡0=1 (Sine and cosine defined by their real power series, The derivatives of sine and cosine are cosine and minus sine).

[L2]

The Pythagorean identity sin⁡2+cos⁡2=1 holds identically, and ∣sin⁡∣≤1, ∣cos⁡∣≤1 (Parity and the Pythagorean identity for sine and cosine).

[L3]

Rotations: SO(3) is the set of R with RTR=I3 and det⁡R=1; products and transposes of elements of SO(3) lie in SO(3) (The orthogonal group O(3) and the rotation group SO(3), SO(3) is a subgroup of the general linear group, with R−1=RT).

[L4]

Moving-frame acceleration identity: for twice continuously differentiable R:I→SO(3), c:I→R3 and y:I→R3, the curve x=Ry+c satisfies RTx′′=y′′+2 ω×y′+ω′×y+ω×(ω×y)+RTc′′, where Ω=RTR′ and ω is the unique vector with Ωz=ω×z for all z (Angular velocity of a moving frame and the rotating-frame acceleration identity). The vector ω is distinct from the scalar rate parameter ω; its components also have dimension τ−1.

[L5]

Galilean kinematics: the coordinate acceleration of a worldline vanishes identically in one inertial frame exactly when it does in every inertial frame (Galilean transformation of worldlines: velocity and acceleration laws, frame-independence of zero coordinate acceleration, and the group of frame changes, clause 3). Inertial frames are the adapted charts of the model, whose spatial basis is constant (Inertial frames, stationary observers and the adopted Galilean transformations between frames).

[L6]

Coordinate velocity and acceleration of a worldline in a frame, and the spatial velocity vector v‾=γ′−u (Coordinate velocity and acceleration of a worldline in an inertial frame, and the spatial velocity and acceleration vectors).

[L7]

Chain rule for total derivatives: if f is totally differentiable at a and g at f(a), then g∘f is totally differentiable at a with D(g∘f)(a)=Dg(f(a))∘Df(a); applied to the compositions s↦sin⁡(ωs) and s↦cos⁡(ωs), whose inner map is linear with derivative ω, it gives the derivatives ωcos⁡(ωs) and −ωsin⁡(ωs) used in step 3.1 (The chain rule for total derivatives: D(g∘f)(a)=Dg(f(a))∘Df(a)).

Verification

technique · direct; verify orthonormality with the Pythagorean identity, then differentiate the coordinate curves explicitly and compare with the cited identity and theorem
1.1L2algebra

The basis field is g-orthonormal for every s: by the expansion and [L2], g(e~1,e~1)=cos⁡2(ωs)+sin⁡2(ωs)=1, g(e~2,e~2)=sin⁡2(ωs)+cos⁡2(ωs)=1, g(e~3,e~3)=1 and g(e~1,e~2)=−cos⁡(ωs)sin⁡(ωs)+sin⁡(ωs)cos⁡(ωs)=0, with the other mixed pairings vanishing; the orientation is unchanged because the determinant of the two-dimensional block is cos⁡2+sin⁡2=1 and the third axis is unchanged.

1.2L6algebra

The worldline γ with F-coordinate curve x(s)=(1,0,0) is a worldline of the model: it is of class C∞ and satisfies the parameter condition, and its coordinate velocity and acceleration in F are w=0 and a=0; its spatial velocity vector in F is v‾=γ′(s)−u=0.

2.1step 1.1L1L3L7algebra

Hence R(s)∈SO(3) for every s: the columns of R(s) are the coordinates of (e~1(s),e~2(s),e~3(s)) and form a positively oriented orthonormal basis, so R(s)TR(s)=I3 and det⁡R(s)=1 by [L3]; moreover sin⁡ and cos⁡ are continuous because differentiable. Inductively, if both are Ck, their derivatives cos⁡ and −sin⁡ are Ck by [L1], so both are Ck+1. Thus they are C∞; composing with s↦ωs by [L7] gives C∞ entries of R and RT.

3.1step 1.2step 2.1L1L2L7algebra

The rotating-basis coordinate curve is y(s)=R(s)Tx(s)=(cos⁡(ωs), −sin⁡(ωs), 0), because R(s)T has first column (cos⁡(ωs),−sin⁡(ωs),0); differentiating with the chain rule [L7] and step 2.1 gives y′(s)=ω(−sin⁡(ωs), −cos⁡(ωs), 0) and y′′(s)=−ω2(cos⁡(ωs), −sin⁡(ωs), 0)=−ω2y(s), so y′′≢0 because y is never the zero vector (its norm is 1 by [L2]).

4.1step 2.1step 3.1L4algebra

The identity of [L4] applies with c=0, x′′=0 and, from Ω=RTR′ computed from the displayed R, with ω the constant vector (0,0,ω); by steps 2.1 and 3.1 the two sides read RTx′′=0 and y′′+2ω×y′+ω′×y+ω×(ω×y)=0, since 2ω×y′=2ω2y, ω′×y=0 and ω×(ω×y)=−ω2y, so the displayed identity is satisfied on this example. Every term has acceleration dimension ℓτ−2; the scalar ω retains the inverse-time dimension declared in the Example.

5.1step 3.1step 4.1L5algebra∎

The result y′′≢0 of step 3.1, together with x′′≡0 in the inertial frame F, shows that the rotating basis is not an inertial frame of the model: were it inertial, its coordinate acceleration of the same worldline would have to vanish identically by clause 3 of [L5], contradicting step 3.1; equivalently, an inertial frame of the model has a constant spatial basis by [L5], and the basis field e~j(s) is not constant. The example therefore delimits the frame assumptions: a time-dependent change of basis preserves simultaneity and the time coordinate but does not preserve the uniform-motion property, and the two extra terms displayed in step 4.1 are kinematic coordinate effects in this basis, not a force law.

Remarks

  • The displayed identity of [L4] shows that in a uniformly rotating basis the second derivative of the coordinate curve has two contributions, the terms proportional to y′ and to y that are familiar from the treatment of rotating frames. The framework at this stage contains no force law, so these terms are kinematic features of the coordinate description; the identification of corresponding terms with fictitious forces belongs to the dynamics of the model, where an equation of motion and a force law are adopted. The example itself makes no such identification.

  • The rotating basis field is not an adapted chart of the affine data, and it is not claimed to be a physical rotation of matter in any sense. The static congruence of observers of the inertial frame F and the rotating basis field are different objects: the observer congruence of Inertial frames, stationary observers and the adopted Galilean transformations between frames is derived from the frame's constant vector fields, while the basis field used here varies with the time coordinate.

Depends on

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