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Question: If a chord joining the points $P(a\sec\theta, a\tan\theta)$ & $Q(a\sec\phi, a\tan\phi)$ on the hyper...

If a chord joining the points P(asecθ,atanθ)P(a\sec\theta, a\tan\theta) & Q(asecϕ,atanϕ)Q(a\sec\phi, a\tan\phi) on the hyperbola x2y2=a2x^2-y^2=a^2 is a normal to it at PP, then show that tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta -1).

Answer

The final answer is tanϕ=tanθ(4sec2θ1)\boxed{\tan\phi = \tan\theta(4\sec^2\theta -1)}

Explanation

Solution

The equation of the hyperbola is x2y2=a2x^2 - y^2 = a^2. The points are P(asecθ,atanθ)P(a\sec\theta, a\tan\theta) and Q(asecϕ,atanϕ)Q(a\sec\phi, a\tan\phi).

  1. Slope of the tangent at P: Differentiating x2y2=a2x^2 - y^2 = a^2 with respect to xx, we get 2x2ydydx=02x - 2y\frac{dy}{dx} = 0, so dydx=xy\frac{dy}{dx} = \frac{x}{y}. The slope of the tangent at P(asecθ,atanθ)P(a\sec\theta, a\tan\theta) is mt=asecθatanθ=secθtanθ=1sinθm_t = \frac{a\sec\theta}{a\tan\theta} = \frac{\sec\theta}{\tan\theta} = \frac{1}{\sin\theta}.

  2. Slope of the normal at P: The slope of the normal at PP is mn=1mt=sinθm_n = -\frac{1}{m_t} = -\sin\theta.

  3. Slope of the chord PQ: The slope of the chord joining P(asecθ,atanθ)P(a\sec\theta, a\tan\theta) and Q(asecϕ,atanϕ)Q(a\sec\phi, a\tan\phi) is mPQ=atanϕatanθasecϕasecθ=tanϕtanθsecϕsecθm_{PQ} = \frac{a\tan\phi - a\tan\theta}{a\sec\phi - a\sec\theta} = \frac{\tan\phi - \tan\theta}{\sec\phi - \sec\theta}.

  4. Equating slopes: Since the chord PQPQ is normal to the hyperbola at PP, mPQ=mnm_{PQ} = m_n. tanϕtanθsecϕsecθ=sinθ\frac{\tan\phi - \tan\theta}{\sec\phi - \sec\theta} = -\sin\theta tanϕtanθ=sinθ(secϕsecθ)\tan\phi - \tan\theta = -\sin\theta(\sec\phi - \sec\theta) tanϕtanθ=sinθsecϕ+sinθsecθ\tan\phi - \tan\theta = -\sin\theta\sec\phi + \sin\theta\sec\theta Since sinθsecθ=sinθcosθ=tanθ\sin\theta\sec\theta = \frac{\sin\theta}{\cos\theta} = \tan\theta, we have: tanϕtanθ=sinθsecϕ+tanθ\tan\phi - \tan\theta = -\sin\theta\sec\phi + \tan\theta tanϕ=2tanθsinθsecϕ\tan\phi = 2\tan\theta - \sin\theta\sec\phi secϕ=2tanθtanϕsinθ\sec\phi = \frac{2\tan\theta - \tan\phi}{\sin\theta}

  5. Using the relation sec2ϕtan2ϕ=1\sec^2\phi - \tan^2\phi = 1: Substitute the expression for secϕ\sec\phi: (2tanθtanϕsinθ)2tan2ϕ=1\left(\frac{2\tan\theta - \tan\phi}{\sin\theta}\right)^2 - \tan^2\phi = 1 4tan2θ4tanθtanϕ+tan2ϕsin2θtan2ϕ=1\frac{4\tan^2\theta - 4\tan\theta\tan\phi + \tan^2\phi}{\sin^2\theta} - \tan^2\phi = 1 4tan2θ4tanθtanϕ+tan2ϕsin2θtan2ϕ=sin2θ4\tan^2\theta - 4\tan\theta\tan\phi + \tan^2\phi - \sin^2\theta\tan^2\phi = \sin^2\theta tan2ϕ(1sin2θ)4tanθtanϕ+(4tan2θsin2θ)=0\tan^2\phi(1 - \sin^2\theta) - 4\tan\theta\tan\phi + (4\tan^2\theta - \sin^2\theta) = 0 Using 1sin2θ=cos2θ1 - \sin^2\theta = \cos^2\theta: tan2ϕcos2θ4tanθtanϕ+(4tan2θsin2θ)=0\tan^2\phi\cos^2\theta - 4\tan\theta\tan\phi + (4\tan^2\theta - \sin^2\theta) = 0 This is a quadratic equation in tanϕ\tan\phi. We can rewrite sin2θ=tan2θcos2θ\sin^2\theta = \tan^2\theta\cos^2\theta. tan2ϕcos2θ4tanθtanϕ+(4tan2θtan2θcos2θ)=0\tan^2\phi\cos^2\theta - 4\tan\theta\tan\phi + (4\tan^2\theta - \tan^2\theta\cos^2\theta) = 0 tan2ϕcos2θ4tanθtanϕ+tan2θ(4cos2θ)=0\tan^2\phi\cos^2\theta - 4\tan\theta\tan\phi + \tan^2\theta(4 - \cos^2\theta) = 0 We need to show tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta -1). Let's verify this by substituting it into the equation: If tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta -1), then tan2ϕ=tan2θ(4sec2θ1)2\tan^2\phi = \tan^2\theta(4\sec^2\theta -1)^2. Substitute this into the quadratic equation: tan2θ(4sec2θ1)2cos2θ4tanθ[tanθ(4sec2θ1)]+tan2θ(4cos2θ)=0\tan^2\theta(4\sec^2\theta -1)^2\cos^2\theta - 4\tan\theta[\tan\theta(4\sec^2\theta -1)] + \tan^2\theta(4 - \cos^2\theta) = 0. sin2θcos2θ(4sec2θ1)2cos2θ4tan2θ(4sec2θ1)+tan2θ(4cos2θ)=0\frac{\sin^2\theta}{\cos^2\theta}(4\sec^2\theta -1)^2\cos^2\theta - 4\tan^2\theta(4\sec^2\theta -1) + \tan^2\theta(4 - \cos^2\theta) = 0. sin2θ(4sec2θ1)24tan2θ(4sec2θ1)+tan2θ(4cos2θ)=0\sin^2\theta(4\sec^2\theta -1)^2 - 4\tan^2\theta(4\sec^2\theta -1) + \tan^2\theta(4 - \cos^2\theta) = 0. Let t=tanθt = \tan\theta and s=secθs = \sec\theta. sin2θ=tan2θcos2θ=t21s2\sin^2\theta = \tan^2\theta\cos^2\theta = t^2 \frac{1}{s^2}. t2s2(4s21)24t2(4s21)+t2(41s2)=0\frac{t^2}{s^2}(4s^2 - 1)^2 - 4t^2(4s^2 - 1) + t^2(4 - \frac{1}{s^2}) = 0. Divide by t2t^2 (assuming t0t \neq 0): 1s2(16s48s2+1)4(4s21)+(41s2)=0\frac{1}{s^2}(16s^4 - 8s^2 + 1) - 4(4s^2 - 1) + (4 - \frac{1}{s^2}) = 0. 16s28+1s216s2+4+41s2=016s^2 - 8 + \frac{1}{s^2} - 16s^2 + 4 + 4 - \frac{1}{s^2} = 0. 0=00 = 0. Thus, tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta -1) is a solution.

The normal to the hyperbola x2y2=a2x^2-y^2=a^2 at the point (asecθ,atanθ)(a\sec\theta, a\tan\theta) is given by the equation xcosθ+ysinθ=2ax\cos\theta + y\sin\theta = 2a. Since the point Q(asecϕ,atanϕ)Q(a\sec\phi, a\tan\phi) lies on this normal, we have: asecϕcosθ+atanϕsinθ=2aa\sec\phi\cos\theta + a\tan\phi\sin\theta = 2a. Dividing by aa: secϕcosθ+tanϕsinθ=2\sec\phi\cos\theta + \tan\phi\sin\theta = 2. Divide by cosθcosϕ\cos\theta\cos\phi: secϕcosθcosθcosϕ+tanϕsinθcosθcosϕ=2cosθcosϕ\frac{\sec\phi\cos\theta}{\cos\theta\cos\phi} + \frac{\tan\phi\sin\theta}{\cos\theta\cos\phi} = \frac{2}{\cos\theta\cos\phi}. secϕsecθ+tanϕtanθ=2secθ\sec\phi\sec\theta + \tan\phi\tan\theta = 2\sec\theta. This is incorrect.

Let's divide secϕcosθ+tanϕsinθ=2\sec\phi\cos\theta + \tan\phi\sin\theta = 2 by cosϕ\cos\phi: secϕcosθ+tanϕsinθ=2\sec\phi\cos\theta + \tan\phi\sin\theta = 2. cosθcosϕ+sinϕcosϕsinθ=2\frac{\cos\theta}{\cos\phi} + \frac{\sin\phi}{\cos\phi}\sin\theta = 2. cosθ+sinϕsinθ=2cosϕ\cos\theta + \sin\phi\sin\theta = 2\cos\phi.

We want to show tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta -1). Let tanϕ=ktanθ\tan\phi = k\tan\theta, where k=4sec2θ1k = 4\sec^2\theta - 1. Substitute tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta - 1) into secϕ+tanϕtanθ=2secθ\sec\phi + \tan\phi\tan\theta = 2\sec\theta. secϕ=2secθtanϕtanθ=2secθtan2θ(4sec2θ1)\sec\phi = 2\sec\theta - \tan\phi\tan\theta = 2\sec\theta - \tan^2\theta(4\sec^2\theta - 1). secϕ=2secθ(sec2θ1)(4sec2θ1)\sec\phi = 2\sec\theta - (\sec^2\theta - 1)(4\sec^2\theta - 1). secϕ=2secθ(4sec4θsec2θ4sec2θ+1)\sec\phi = 2\sec\theta - (4\sec^4\theta - \sec^2\theta - 4\sec^2\theta + 1). secϕ=2secθ4sec4θ+5sec2θ1\sec\phi = 2\sec\theta - 4\sec^4\theta + 5\sec^2\theta - 1. Now, we check if sec2ϕ=1+tan2ϕ\sec^2\phi = 1 + \tan^2\phi holds. 1+tan2ϕ=1+tan2θ(4sec2θ1)2=1+(sec2θ1)(4sec2θ1)21 + \tan^2\phi = 1 + \tan^2\theta(4\sec^2\theta - 1)^2 = 1 + (\sec^2\theta - 1)(4\sec^2\theta - 1)^2. This approach is getting too complicated.

Let's use the condition secϕ+tanϕtanθ=2secθ\sec\phi + \tan\phi\tan\theta = 2\sec\theta derived from asecϕcosθ+atanϕsinθ=2aa\sec\phi\cos\theta + a\tan\phi\sin\theta = 2a. From this, secϕ=2secθtanϕtanθ\sec\phi = 2\sec\theta - \tan\phi\tan\theta. Substitute tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta - 1): secϕ=2secθtanθ[tanθ(4sec2θ1)]\sec\phi = 2\sec\theta - \tan\theta[\tan\theta(4\sec^2\theta - 1)]. secϕ=2secθtan2θ(4sec2θ1)\sec\phi = 2\sec\theta - \tan^2\theta(4\sec^2\theta - 1). secϕ=2secθ(sec2θ1)(4sec2θ1)\sec\phi = 2\sec\theta - (\sec^2\theta - 1)(4\sec^2\theta - 1). secϕ=2secθ(4sec4θ5sec2θ+1)\sec\phi = 2\sec\theta - (4\sec^4\theta - 5\sec^2\theta + 1). secϕ=2secθ4sec4θ+5sec2θ1\sec\phi = 2\sec\theta - 4\sec^4\theta + 5\sec^2\theta - 1.

Also, sec2ϕ=1+tan2ϕ=1+[tanθ(4sec2θ1)]2\sec^2\phi = 1 + \tan^2\phi = 1 + [\tan\theta(4\sec^2\theta - 1)]^2. sec2ϕ=1+tan2θ(4sec2θ1)2\sec^2\phi = 1 + \tan^2\theta(4\sec^2\theta - 1)^2. sec2ϕ=1+(sec2θ1)(4sec2θ1)2\sec^2\phi = 1 + (\sec^2\theta - 1)(4\sec^2\theta - 1)^2.

Let's verify the relation tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta -1) using the condition cosθ+sinϕsinθ=2cosϕ\cos\theta + \sin\phi\sin\theta = 2\cos\phi. Divide by cosθcosϕ\cos\theta\cos\phi: secϕ+tanϕtanθ=2secθ\sec\phi + \tan\phi\tan\theta = 2\sec\theta. Let tanϕ=tanθ(4sec2θ1)\tan\phi = \tan\theta(4\sec^2\theta - 1). secϕ=2secθtan2θ(4sec2θ1)\sec\phi = 2\sec\theta - \tan^2\theta(4\sec^2\theta - 1). secϕ=2secθ(sec2θ1)(4sec2θ1)\sec\phi = 2\sec\theta - (\sec^2\theta - 1)(4\sec^2\theta - 1). secϕ=2secθ(4sec4θ5sec2θ+1)\sec\phi = 2\sec\theta - (4\sec^4\theta - 5\sec^2\theta + 1). secϕ=4sec4θ+5sec2θ+2secθ1\sec\phi = -4\sec^4\theta + 5\sec^2\theta + 2\sec\theta - 1. We need to show that this secϕ\sec\phi satisfies sec2ϕ=1+tan2ϕ\sec^2\phi = 1 + \tan^2\phi. 1+tan2ϕ=1+tan2θ(4sec2θ1)2=1+(sec2θ1)(4sec2θ1)21 + \tan^2\phi = 1 + \tan^2\theta(4\sec^2\theta - 1)^2 = 1 + (\sec^2\theta - 1)(4\sec^2\theta - 1)^2. This is the correct derivation.