Comprehensive Study Notes on Related Rates

Fundamentals of Related Rates

  • Core Definition: Related rates is a calculus technique used to analyze how variables in a formula change with respect to time (tt). It relates the known rates of change of certain quantities to derive an unknown rate of change of another quantity at a specific instant.

  • Primary Objective: To find the instantaneous rate of change of a geometric, physical, or economic quantity at a precise moment (e.g., determining the exact expansion velocity of a volume at t=3secondst = 3_\text{seconds}).

  • Implicit Functions of Time: Variables such as volume (VV), radius (rr), height (hh), area (AA), distance (xx, yy), or angle (θ\theta) are treated as implicit functions of time (tt).

  • Implicit Differentiation Requirement: Because these quantities are functions of tt, taking the derivative of an equation containing these variables with respect to tt requires applying the chain rule. Differentiating any variable vv with respect to tt produces an accompanying differential term dvdt\frac{dv}{dt}.

General Four-Step Procedure for Related Rates Problems

  • Step 1: Define Variables and Constants: Assign distinct symbols to all time-varying quantities and identify all constant values present in the system (e.g., assign tt for time, AA for area, rr for radius, hh for height, θ\theta for angle of elevation).

  • Step 2: Formulate the Primary Relational Equation: Identify or derive a geometric, physical, or trigonometric formula that links all non-time variables together.

  • Step 3: Implicitly Differentiate with Respect to Time (tt): Apply the differential operator ddt\frac{d}{dt} to both sides of the relational formula. Use differentiation rules (product rule, quotient rule, chain rule, power rule) as required, ensuring that every differentiated variable term generates a corresponding d[variable]dt\frac{d[\text{variable}]}{dt} differential factor.

  • Step 4: Substitute Known Instantaneous Values and Solve: Plug in all given static values (distances, heights, radii) and known rates of change corresponding to the specific moment in time into the differentiated equation. Solve algebraically for the targeted unknown rate of change.

Mathematical Derivation: Volume Change in a Conical Reservoir

  • Geometric Background and Formulas:

    • Area of a circle:         A=πr2A = \pi r^2

    • Volume of a cylinder (a stack of circular cross-sections across height hh):         V=πr2hV = \pi r^2 h

    • Volume of a cone (one-third the volume of a cylinder with equivalent base and height):         V=13πr2hV = \frac{1}{3}\pi r^2 h         V=π3r2hV = \frac{\pi}{3} r^2 h

  • Dynamic System Model:

    • Consider a conical reservoir positioned under a water faucet. Water enters to a certain height hh and radius rr. If a hole is opened at the apex/bottom of the cone, water drains out.

    • As water leaves the cone, the water level drops, causing both the liquid's height hh and upper radius rr to decrease continuously over time tt.

    • Because VV, rr, and hh vary dynamically with time, all three are explicit functions of time: V(t)V(t), r(t)r(t), and h(t)h(t).

  • Implicit Differentiation wrt Time (tt):

    • Apply ddt\frac{d}{dt} to both sides of the conical volume formula:         ddt(V)=ddt(π3r2h)\frac{d}{dt}(V) = \frac{d}{dt}\left(\frac{\pi}{3} r^2 h\right)

    • The left side yields dVdt\frac{dV}{dt}, representing the instantaneous rate of change of volume with respect to time.

    • The right side requires the product rule between r2r^2 and hh, treating π3\frac{\pi}{3} as a constant factor:         dVdt=π3((ddt(r2))h+r2(ddt(h)))\frac{dV}{dt} = \frac{\pi}{3} \left( \left(\frac{d}{dt}(r^2)\right) h + r^2 \left(\frac{d}{dt}(h)\right) \right)

    • Applying the chain rule yields:         ddt(r2)=2rdrdt\frac{d}{dt}(r^2) = 2r \frac{dr}{dt}         ddt(h)=dhdt\frac{d}{dt}(h) = \frac{dh}{dt}

    • Combining these results yields the complete expanded equation:         dVdt=π3(2rhdrdt+r2dhdt)\frac{dV}{dt} = \frac{\pi}{3} \left( 2r h \frac{dr}{dt} + r^2 \frac{dh}{dt} \right)         dVdt=2π3rhdrdt+π3r2dhdt\frac{dV}{dt} = \frac{2\pi}{3} r h \frac{dr}{dt} + \frac{\pi}{3} r^2 \frac{dh}{dt}

  • Necessary Data for Instantaneous Evaluation:     To evaluate dVdt\frac{dV}{dt} at a specific instant, four independent pieces of information must be known:

    1. Instantaneous radius (rr)

    2. Instantaneous height (hh)

    3. Instantaneous rate of change of radius (drdt\frac{dr}{dt})

    4. Instantaneous rate of change of height (dhdt\frac{dh}{dt})

Basic Algebraic Related Rates Examples

  • Implicit Differentiation of y=x3y = x^3:

    • Given y=x3y = x^3, where both xx and yy are dynamic functions of time tt.

    • Differentiate both sides with respect to tt:         ddt(y)=ddt(x3)\frac{d}{dt}(y) = \frac{d}{dt}(x^3)         dydt=3x2dxdt\frac{dy}{dt} = 3x^2 \frac{dx}{dt}

  • Evaluation at Specific Instant (t=1t = 1):

    • Given conditions at t=1t = 1: x=2x = 2 and dxdt=4units/s\frac{dx}{dt} = 4_\text{units/s}.

    • Note: Quantitative parameters (xx and dxdt\frac{dx}{dt}) are context-dependent and change over time; values given for t=1t = 1 apply strictly to that moment.

    • Substitute values into the differentiated formula:         dydt=3(2)2×4\frac{dy}{dt} = 3(2)^2 \times 4         dydt=3(4)×4\frac{dy}{dt} = 3(4) \times 4         dydt=48units/s\frac{dy}{dt} = 48_\text{units/s}

    • Interpretation: At time t=1t = 1, yy increases at an instantaneous rate of 48units48_\text{units} per unit of time.

Geometric Application: Circular Oil Spill Expansion

  • Problem Statement: An oil tanker spill (modeled on events such as the Exxon Valdez incident) creates a thin circular slick on the surface of the water. The radius of the circular slick expands at a constant rate of 3ft/s3_\text{ft/s}. Determine the rate at which the surface area of the spill is increasing at the exact instant when the radius reaches 30ft30_\text{ft}.

  • Identified Variables and Given Rates:

    • Time: tt

    • Radius: r=30ftr = 30_\text{ft}

    • Area: AA

    • Rate of radius expansion: drdt=3ft/s\frac{dr}{dt} = 3_\text{ft/s}

  • Relating Formula:

    • Area of a circle:         A=πr2A = \pi r^2

  • Implicit Differentiation:

    • Differentiate with respect to tt:         dAdt=2πrdrdt\frac{dA}{dt} = 2\pi r \frac{dr}{dt}

  • Computation:

    • Substitute r=30ftr = 30_\text{ft} and drdt=3ft/s\frac{dr}{dt} = 3_\text{ft/s}:         dAdt=2π(30ft)×3ft/s\frac{dA}{dt} = 2\pi (30_\text{ft}) \times 3_\text{ft/s}         dAdt=180πft2/s\frac{dA}{dt} = 180\pi_\text{ft}^2/\text{s}

  • Dimensional Verification & Numerical Result:

    • Units match surface area growth: ft×ft/s=ft2/s\text{ft} \times \text{ft/s} = \text{ft}^2/\text{s}.

    • Exact rate of area expansion: 180πft2/s180\pi_\text{ft}^2/\text{s}.

    • Decimal approximation: 180×3.14159265...≈565.49ft2/s180 \times 3.14159265... \approx 565.49_\text{ft}^2/\text{s}.

Trigonometric Application: Tracking Camera Angle for a Rocket Launch

  • Problem Setup: A rocket ascends vertically from a launchpad. An automated television tracking camera is situated at ground level at a fixed distance of 3000ft3000_\text{ft} from the launch point.

  • Target Condition: When the rocket reaches an altitude of h=4000fth = 4000_\text{ft}, its climbing speed is dhdt=600ft/s\frac{dh}{dt} = 600_\text{ft/s}. Calculate the required angular velocity dθdt\frac{d\theta}{dt} of the tracking camera at that moment to keep the rocket centered in the frame.

  • Assigned Variables:

    • Time: tt

    • Rocket Height / Altitude: hh

    • Camera Angle of Elevation: θ\theta

    • Horizontal Camera Distance (constant): 3000ft3000_\text{ft}

  • Formula Selection:

    • The Pythagorean theorem (a2+b2=c2a^2 + b^2 = c^2) relates side lengths but omits the camera angle θ\theta.

    • The tangent trigonometric ratio connects angle θ\theta, opposite side hh, and adjacent side 3000ft3000_\text{ft}:         tan⁡(θ)=oppositeadjacent=h3000\tan(\theta) = \frac{\text{opposite}}{\text{adjacent}} = \frac{h}{3000}         tan⁡(θ)=13000h\tan(\theta) = \frac{1}{3000}h

  • Implicit Differentiation:

    • Differentiate both sides with respect to tt:         ddt(tan⁡(θ))=ddt(13000h)\frac{d}{dt}(\tan(\theta)) = \frac{d}{dt}\left(\frac{1}{3000}h\right)         sec⁡2(θ)dθdt=13000dhdt\sec^2(\theta) \frac{d\theta}{dt} = \frac{1}{3000} \frac{dh}{dt}

  • Geometric Evaluation at Instant h=4000fth = 4000_\text{ft}:

    • The camera, launch site, and rocket form a right triangle with adjacent side 3000ft3000_\text{ft} and opposite side 4000ft4000_\text{ft}.

    • Calculate hypotenuse cc using the Pythagorean theorem:         c=30002+40002=9000000+16000000=25000000=5000ftc = \sqrt{3000^2 + 4000^2} = \sqrt{9000000 + 16000000} = \sqrt{25000000} = 5000_\text{ft}

    • Determine cos⁡(θ)\cos(\theta):         cos⁡(θ)=adjacenthypotenuse=30005000=35\cos(\theta) = \frac{\text{adjacent}}{\text{hypotenuse}} = \frac{3000}{5000} = \frac{3}{5}

    • Determine sec⁡(θ)\sec(\theta) (reciprocal of cosine):         sec⁡(θ)=1cos⁡(θ)=53\sec(\theta) = \frac{1}{\cos(\theta)} = \frac{5}{3}

    • Determine sec⁡2(θ)\sec^2(\theta):         sec⁡2(θ)=(53)2=259\sec^2(\theta) = \left(\frac{5}{3}\right)^2 = \frac{25}{9}

  • Substitution and Algebraic Solution:

    • Substitute sec⁡2(θ)=259\sec^2(\theta) = \frac{25}{9} and dhdt=600ft/s\frac{dh}{dt} = 600_\text{ft/s} into the differentiated formula:         259dθdt=13000(600)\frac{25}{9} \frac{d\theta}{dt} = \frac{1}{3000} (600)         259dθdt=15\frac{25}{9} \frac{d\theta}{dt} = \frac{1}{5}

    • Isolate dθdt\frac{d\theta}{dt} by multiplying both sides by 925\frac{9}{25}:         dθdt=15×925\frac{d\theta}{dt} = \frac{1}{5} \times \frac{9}{25}         dθdt=9125rad/s=0.072rad/s\frac{d\theta}{dt} = \frac{9}{125}_\text{rad/s} = 0.072_\text{rad/s}

  • Conversion to Degrees per Second:

    • Convert radians per second to degrees per second using the conversion factor 180∘π\frac{180^\circ}{\pi}:         dθdt=0.072×180∘π\frac{d\theta}{dt} = 0.072 \times \frac{180^\circ}{\pi}         dθdt=12.96π≈4.1253∘/s≈4.13∘/s\frac{d\theta}{dt} = \frac{12.96}{\pi} \approx 4.1253^\circ/\text{s} \approx 4.13^\circ/\text{s}

  • Final Interpretation: At the moment the rocket reaches an altitude of 4000ft4000_\text{ft}, the tracking camera must tilt upwards at an instantaneous angular velocity of 0.072rad/s0.072_\text{rad/s} (approximately 4.13∘/s4.13^\circ/\text{s}) to keep the rocket centered in view.