Q.If A=[0tan2α−tan2α0], then show that I+A=(I−A)[cosαsinα−sinαcosα], where I is the identity matrix of order 2.
OR
If A=12323−3−32−4, then find A−1; and hence solve the system of equations x+2y−3z=−4, 2x+3y+2z=2, 3x−3y−4z=11.
Assam AhsecAHSEC Higher Secondary (HS) Final Examination 2019Subjective· 6mImportance★★★★★
A rotation in the plane is usually written with trigonometry:
Rθ=(cosθsinθ−sinθcosθ).
The Cayley transform produces the same rotation using only addition, multiplication and division — no sine or cosine at all.
The idea
Start from the skew-symmetric matrix
S=(0t−t0).
Its Cayley transform is
C(S)=(I+S)(I−S)−1=1+t21(1−t22t−2t1−t2).
This C(S) is orthogonal with determinant +1, so it is a genuine rotation matrix. Its angle ϕ satisfies
tan2ϕ=t,ϕ=2arctant.
So the parameter t is not the rotation angle — it is the tangent of the half angle.
Important
The single fact to hold on to: t=tan(ϕ/2), not the angle itself.
Note
Order matters. Here I+S and I−S commute, so (I+S)(I−S)−1 and (I−S)−1(I+S) give the same matrix. Writing the factors the other way round, (I−S)(I+S)−1, would instead produce the clockwise rotation R−ϕ.
Main: multiply out (I−A)R where R is the given rotation-like matrix, using t=tan2α half-angle formulas for cosα,sinα; every entry matches I+A. OR: compute detA, the adjugate, hence A−1, then solve AX=B via X=A−1B. …
Main: multiply out (I−A)R where R is the given rotation-like matrix, using t=tan2α half-angle formulas for cosα,sinα; every entry matches I+A. OR: compute detA, the adjugate, hence A−1, then solve AX=B via X=A−1B.
Main question.A=[0tan2α−tan2α0]. Let t=tan2α, so A=[0t−t0].
I+A=[1t−t1],I−A=[1−tt1].
Recall the half-angle identities: cosα=1+t21−t2, sinα=1+t22t.
Compute (I−A)[cosαsinα−sinαcosα] entrywise (row of I−A dotted with column of the rotation matrix):