Part A
Alright, let's break this down. The first step is to find the signal strength at the two endpoints of our interval: t=0 and t=6. This is a two-step process: first find the distance d at each time, then find the signal strength S for that distance.
At t = 0:
d(0) = 42000 + 1500sin((π/12) * 0) = 42000 + 1500sin(0) = 42000 km.
S(d(0)) = S(42000) = (5 * 10^6) / (42000 - 38000) = (5 * 10^6) / 4000 = 1250 SU.
At t = 6:
d(6) = 42000 + 1500sin((π/12) * 6) = 42000 + 1500sin(π/2) = 42000 + 1500(1) = 43500 km.
S(d(6)) = S(43500) = (5 * 10^6) / (43500 - 38000) = (5 * 10^6) / 5500 ≈ 909.091 SU.
Now, we can calculate the average rate of change using the classic slope formula:
Average Rate of Change = (S(6) - S(0)) / (6 - 0)
= (909.091 - 1250) / 6 = -340.909 / 6 ≈ -56.818
Interpretation: Between midnight (t=0) and 6 AM (t=6), the signal strength from the satellite is decreasing, on average, at a rate of approximately 56.818 signal units per hour.
Part B
This is a great question that tests your understanding of composite functions. The key is to think about the 'inside' function, d(t), first.
d(t) is a sinusoidal function, which means it oscillates forever. It never settles on a single value. It will always oscillate between its minimum value (42000 - 1500 = 40500 km) and its maximum value (42000 + 1500 = 43500 km).
Because the input to the S(d) function is constantly oscillating, the output, S(t), will also constantly oscillate. Therefore, S(t) does not have a single, constant end behavior as t → ∞.
Instead, its long-run behavior is to oscillate between a minimum and maximum value. We can find these values:
- Max Signal Strength: Occurs at min distance (
d=40500). S(40500) = (5*10^6)/(40500-38000) = 2000 SU.
- Min Signal Strength: Occurs at max distance (
d=43500). S(43500) = (5*10^6)/(43500-38000) ≈ 909.091 SU.
So, for all time, the signal strength S(t) will oscillate between approximately 909.1 SU and 2000 SU.
Part C
To maximize the signal strength S(d) = (5 * 10^6) / (d - 38000), we need to make the denominator as small as possible. This happens when the distance, d(t), is at its minimum.
The minimum value of the sine function is -1. So, we need to find the time t when sin((π/12)t) = -1.
sin(θ) = -1 when θ = 3π/2, 7π/2, ...
Let (π/12)t = 3π/2.
Solving for t: t = (3π/2) * (12/π) = 18.
So, the first time after t=0 that the signal is strongest is at t = 18 hours.
The maximum signal strength occurs at this time, when the distance is at its minimum (d = 42000 + 1500(-1) = 40500 km).
Maximum S = S(40500) = (5 * 10^6) / (40500 - 38000) = (5 * 10^6) / 2500 = 2000 SU.
Part D
This is where we put it all together. We need to find the times t when S(t) ≥ 1600.
First, let's set up the inequality:
(5 * 10^6) / (d(t) - 38000) ≥ 1600
We know from the problem setup that the minimum distance is 40500 km, so the denominator (d(t) - 38000) is always positive. This means we can multiply both sides by it without flipping the inequality sign. This is a common mistake, so be careful!
5 * 10^6 ≥ 1600 * (d(t) - 38000)
3125 ≥ d(t) - 38000
41125 ≥ d(t)
So, the signal is strong enough whenever the satellite's distance is less than or equal to 41,125 km. Now we substitute the function for d(t):
41125 ≥ 42000 + 1500sin((π/12)t)
-875 ≥ 1500sin((π/12)t)
-875 / 1500 ≥ sin((π/12)t)
-0.5833 ≥ sin((π/12)t)
Let θ = (π/12)t. We need to find where sin(θ) ≤ -0.5833. The sine function is negative in Quadrants III and IV.
First, find the reference angle: θ_ref = arcsin(0.5833) ≈ 0.6228 radians.
The boundaries for our solution in the interval [0, 2π] are:
θ₁ = π + θ_ref = π + 0.6228 ≈ 3.7644
θ₂ = 2π - θ_ref = 2π - 0.6228 ≈ 5.6604
Since we need sin(θ) to be less than -0.5833, the solution is the interval between these two angles: 3.7644 ≤ θ ≤ 5.6604.
Now, substitute back θ = (π/12)t:
3.7644 ≤ (π/12)t ≤ 5.6604
Finally, solve for t by multiplying by 12/π:
(12/π) * 3.7644 ≤ t ≤ (12/π) * 5.6604
14.38 ≤ t ≤ 21.62
The signal is strong enough during the time interval [14.38, 21.62] hours.