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An aircraft flies 50 km on a bearing of 065 degrees, then 80 km on a bearing of 040 degrees. Calculate the total distance of the aircraft from its starting point.

Mathematics

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Answer

127.1 km\text{127.1 km}

049.6∘\text{049.6}^\circ

Step-by-step solution

5 steps
  1. Calculate the North and East components for the first leg.

    The aircraft flies 50 km50 \text{ km} on a bearing of 065∘065^\circ.
    Let N1N_1 be the North component and E1E_1 be the East component.

    N1=50cos⁡(65∘)N_1 = 50 \cos(65^\circ) E1=50sin⁡(65∘)E_1 = 50 \sin(65^\circ)

    Using a calculator:

    N1≈50×0.4226=21.13 kmN_1 \approx 50 \times 0.4226 = 21.13 \text{ km} E1≈50×0.9063=45.32 kmE_1 \approx 50 \times 0.9063 = 45.32 \text{ km}
  2. Calculate the North and East components for the second leg.

    From the end of the first leg, the aircraft flies 80 km80 \text{ km} on a bearing of 040∘040^\circ.
    Let N2N_2 be the North component and E2E_2 be the East component.

    N2=80cos⁡(40∘)N_2 = 80 \cos(40^\circ) E2=80sin⁡(40∘)E_2 = 80 \sin(40^\circ)

    Using a calculator:

    N2≈80×0.7660=61.28 kmN_2 \approx 80 \times 0.7660 = 61.28 \text{ km} E2≈80×0.6428=51.42 kmE_2 \approx 80 \times 0.6428 = 51.42 \text{ km}
  3. Calculate the total North and East displacement from the aerodrome A.

    Let NtotalN_{total} be the total North displacement and EtotalE_{total} be the total East displacement.

    Ntotal=N1+N2=21.13 km+61.28 km=82.41 kmN_{total} = N_1 + N_2 = 21.13 \text{ km} + 61.28 \text{ km} = 82.41 \text{ km} Etotal=E1+E2=45.32 km+51.42 km=96.74 kmE_{total} = E_1 + E_2 = 45.32 \text{ km} + 51.42 \text{ km} = 96.74 \text{ km}
  4. Calculate the distance of the aircraft from A.

    The distance from A is the hypotenuse of the right-angled triangle formed by NtotalN_{total} and EtotalE_{total}.

    Distance=Ntotal2+Etotal2\text{Distance} = \sqrt{N_{total}^2 + E_{total}^2} Distance=(82.41)2+(96.74)2\text{Distance} = \sqrt{(82.41)^2 + (96.74)^2} Distance=6791.4081+9358.6276\text{Distance} = \sqrt{6791.4081 + 9358.6276} Distance=16150.0357\text{Distance} = \sqrt{16150.0357} Distance≈127.08 km\text{Distance} \approx 127.08 \text{ km}

    Rounding to one decimal place:

    Distance≈127.1 km\text{Distance} \approx 127.1 \text{ km}
  5. Calculate the bearing of the aircraft from A.

    Let θ\theta be the angle measured clockwise from the North line.

    tan⁡(θ)=EtotalNtotal\tan(\theta) = \frac{E_{total}}{N_{total}} tan⁡(θ)=96.7482.41\tan(\theta) = \frac{96.74}{82.41} tan⁡(θ)≈1.1739\tan(\theta) \approx 1.1739 θ=arctan⁡(1.1739)\theta = \arctan(1.1739) θ≈49.57∘\theta \approx 49.57^\circ

    Since both NtotalN_{total} and EtotalE_{total} are positive, the aircraft is in the North-East quadrant, so the bearing is simply this angle.
    Rounding to one decimal place and expressing as a 3-digit bearing:

    Bearing≈049.6∘\text{Bearing} \approx 049.6^\circ

    The distance of the aircraft from A is 127.1 km\boxed{\text{127.1 km}} and its bearing from A is 049.6∘\boxed{\text{049.6}^\circ}.

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