Problem Overview
We linearize the quadcopter flight path y(x)=4xβx2 at waypoint x=3 and evaluate local path estimation accuracy.
Step-by-Step Mathematical Solution
Step 1: Compute General Derivative yβ²(x)
Set up the difference quotient limit:
yβ²(x)=hβ0limβh[4(x+h)β(x+h)2]β(4xβx2)β
=hβ0limβh4x+4hβ(x2+2xh+h2)β4x+x2β
=hβ0limβh4hβ2xhβh2β=hβ0limβ(4β2xβh)=4β2x
Step 2: Evaluate Point of Tangency and Slope at x=3
- Altitude coordinate:
y(3)=4(3)β(3)2=12β9=3Β mβΉ(3,3)
- Instantaneous tangent slope:
m=yβ²(3)=4β2(3)=4β6=β2
Step 3: Construct the Tangent Line (Linearization L(x))
Using point-slope form yβy1β=m(xβx1β):
yβ3=β2(xβ3)βΉyβ3=β2x+6
L(x)=β2x+9
Step 4: Compare Linear Approximation with Exact Nonlinear Value at x=3.1
- Linear Tangent Approximation:
L(3.1)=β2(3.1)+9=β6.2+9=2.80Β m
- Exact Trajectory Value:
y(3.1)=4(3.1)β(3.1)2=12.4β9.61=2.79Β m
- Approximation Error:
Error=β£2.79β2.80β£=0.01Β m(β0.36%Β relativeΒ error)
Engineering Conclusion
Within a narrow window near x=3, the tangent line linearization L(x)=β2x+9 predicts the vehicle position to within 1Β centimeter of accuracy. In robotics and embedded flight control, substituting tangent line models for nonlinear curves allows low-power flight microprocessors to execute guidance loop corrections at over 500Β Hz without computational latency.