A linear model (equation) can be written in the following, equivalent forms.
The second form can be solved for y which will make it look like the first form. The models in this section will be in the first form which you may know as slope intercept. The \(m\) is commonly described as the slope which is a measure of how steep the line is. In these models we will generalize slope to a rate. The \(b\) is commonly called the intercept which indicates a shift of the line up or down. This shift will have a meaning in each application.
Before we use this model, we need to figure out what each part is.
\(T_G\) is a parameter that we need to find before we use the model. A parameter is not a variable, rather it is a value (number) that we obtain from the circumstances and write into the model (equation) before we do any work.
In contrast the ratio
\(-\frac{3.5^\circ}{1000 \text{ ft}}\) is a constant (not a parameter), because it is a result of atmospheric physics. This ratio is always in the equation, because it is not dependent on the location for this simplified model.
The model subtracting from the starting temperature results in a decrease of temperature from
\(T_G\text{.}\) This implies that temperature decreases with altitude.
Example 3.1.2.
If the temperature at ground level is 43Β° what is the temperature 1000 ft above ground level (AGL)? 2000 ft AGL, 3000 ft AGL, 3500 ft AGL?
Because fractions of a degree are not useful in making decisions like what clothes to wear, we will round to units.
Note \(T_G = 43^\circ\text{.}\) We need to calculate \(T_A\) for \(A=1000, 2000, 3000, 3500\text{.}\)
\begin{align*}
T_{1000} & = 43^\circ - \frac{3.5^\circ}{1000 \text{ ft}}(1000 \text{ ft})\\
& = 39.5\\
& = 43^\circ - 3.5^\circ\\
& = 39.5\\
& \approx 40.\\
T_{2000} & = 43^\circ - \frac{3.5^\circ}{1000 \text{ ft}}(2000 \text{ ft})\\
& = 43^\circ - 7.0^\circ\\
& = 36.\\
T_{3000} & = 43^\circ - \frac{3.5^\circ}{1000 \text{ ft}}(3000 \text{ ft})\\
& = 43^\circ - 10.5^\circ\\
& = 32.5\\
& \approx 33.\\
T_{3500} & = 43^\circ - \frac{3.5^\circ}{1000 \text{ ft}}(3500 \text{ ft})\\
& = 43^\circ - 12.25^\circ\\
& = 30.75\\
& \approx 31.
\end{align*}
Notice that we now know that it will be below freezing just above 3000 ft.
An Equation for Time to Altitude.
A fixed wing aircraft flown optimally climbs from a starting altitude at a fixed climb rate.
\begin{equation*}
A_t = A_G+C \cdot t.
\end{equation*}
-
\(A_t\) is the altitude after \(t\) minutes.
-
\(A_G\) is the starting altitude (likely ground level) in feet mean sea level (MSL).
-
\(C\) is the rate of climb in feet per minute.
-
\(t\) is the time since the climb began in minutes.
Before we can use this equation, letβs analyze it. We will need to know the parameters
\(A_G\) and
\(C\text{.}\) A parameter is not a variable, rather it is a value (number) that we obtain from the circumstances and write into the model (equation) before we do any work.
\(A_G\) varies by airport, because they are at different altitudes. The rate
\(C\) must be obtained for each plane and is often available in the aircraftβs Pilotβs Operating Handbook (POH).
Final altitude (
\(A_t\)) and time (
\(t\)) are the variables which implies that the model shows a relationship between time climbing and how high the plane is.
In this model everything is added which matches the increase of elevation over time (adding makes the altitude bigger).
Every linear model (equation) has a rate (the slope
\(m\) in the equation). In this case
\(m=\frac{C \text{ ft}}{1 \text{ min}}\text{.}\) Every linear model has a shift (the
\(b\) in the equation), which may be zero. In this case
\(b=A_G\text{.}\) \(b=A_G=0\) is possible because an aircraft can take off from sea level (e.g., float planes). This shift makes sense, because the climb starts at the altitude of the ground: the plane was already shifted up by being at that airport.
Now that we have analyzed this equation, we are prepared to use it.
Example 3.1.3.
If a plane begins at 160 ft MSL and is climbing at 700 ft/min, how high will it be after 5 minutes? 10 minutes? 15 minutes?
These calculations are made as part of safety planning. The data is sufficiently accurate that rounding is not necessary. Rather we make conservative estimates of the parameters, so that there is always a safety buffer. In this case a conservative estimate for
\(A_G\) is to round down: this will give us a lower altitude. If that lower altitude is safe, then altitude 5 feet higher will be safe as well. For the climb rate a conservative estimate is to round down as well. If we can reach an altitude climbing at 700 ft/min, then if we climb at 720 ft/min we will reach that safe altitude a little sooner.
Note
\begin{equation*}
A_t = 160 \text{ ft}+\frac{700 \text{ ft}}{\text{min}} \cdot t.
\end{equation*}
The expected altitudes are
\begin{align*}
A_5 & = 160 \text{ ft}+\frac{700 \text{ ft}}{\text{min}} \cdot 5 \text{ min}\\
& = 160 \text{ ft}+3500 \text{ ft}\\
& = 3660.\\
A_{10} & = 160 \text{ ft}+\frac{700 \text{ ft}}{\text{min}} \cdot 10 \text{ min}\\
& = 160 \text{ ft}+7000 \text{ ft}\\
& = 7160.\\
A_{15} & = 160 \text{ ft}+\frac{700 \text{ ft}}{\text{min}} \cdot 15 \text{ min}\\
& = 160 \text{ ft}+10500 \text{ ft}\\
& = 10660.
\end{align*}
Based on these calculations the plane will climb above 4500 ft MSL in between 5 and 10 minutes (closer to 5).
Equation for Fuel Remaining.
When operated at a fixed power setting a vehicle burns the same amount of gas per hour (or other time unit). This leads to the linear model
\begin{equation*}
F_t = F_I - r \cdot t.
\end{equation*}
-
\(F_t\) is the amount of fuel remaining after \(t\) minutes.
-
\(F_I\) is the amount of fuel at the beginning.
-
\(r\) is the rate (volume per time) at which fuel is being consumed.
-
\(t\) is the time the vehicle has been operated.
Fuel amounts will be measured in units of volume like gallons or liters. Time will be measured in minutes or hours. The rate \(r\) is then in units such as gallons/hour or liters/min.
Before we use this model, letβs analyze it. We will need to know the parameters
\(F_I\) and
\(r\text{.}\) These parameters are not variables (they remains the same the whole time the model is in use), rather they are values (numbers) that we obtain from the circumstances and write into the model (equation) before we do any work.
The initial fuel
\(F_I\) is obtained by checking the fuel tanks or fuel gauges. The rate
\(r\) is often is not shown during operation (fuel gauges show how much is remaining rather than how fast it is used). The rate can sometimes be obtained from vehicle documentation.
Final fuel (
\(F_t\)) and time (
\(t\)) are the variables which implies that the model shows a relationship between time flown and fuel available (left in the tanks).
Because fuel decreases the
\(r \cdot t\) term is subtracted decreasing the amount from
\(F_I\text{.}\)
Every linear model (equation) has a rate. In this case
\(m=\frac{r \text{ gal}}{1 \text{ hr}}\) (or similar units).
Every linear model has a shift. In this case
\(b=F_I\text{.}\) We can think of this shift in terms of the needle on the gas gauge moving up to represent the amount of fuel present.
Now that we have analyzed this equation, we are prepared to use it.
Example 3.1.4.
If a car begins with 20 gallons of fuel and burns 1.55 gallons per hour, how much fuel will it have after 1 hour, 2 hours, 3 hours, 36 minutes?
A gallon is a large amount so we will maintain one decimal place precision. For safety we should always assume a larger fuel burn, so we will round fuel remaining down.
Solution.
The model is
\begin{equation*}
F_t = 20 \text{ gal} - \frac{1.55 \text{ gal}}{\text{hr}} \cdot t \text{ hr}\text{.}
\end{equation*}
Thus
\begin{align*}
F_1 & = 20 \text{ gal} - \frac{1.55 \text{ gal}}{\text{hr}} \cdot 1 \text{ hr}\\
& = 20 \text{ gal} - 1.55 \text{ gal}\\
& = 18.45\\
& \approx 18.4.\\
F_2 & = 20 \text{ gal} - \frac{1.55 \text{ gal}}{\text{hr}} \cdot 2 \text{ hrs}\\
& = 20 \text{ gal} - 3.10 \text{ gal}\\
& = 16.9.\\
F_3 & = 20 \text{ gal} - \frac{1.55 \text{ gal}}{\text{hr}} \cdot 3 \text{ hrs}\\
& = 20 \text{ gal} - 4.65 \text{ gal}\\
& = 15.35\\
& \approx 15.3.\\
F_{0.6} & = 20 \text{ gal} - \frac{1.55 \text{ gal}}{\text{hr}} \cdot 0.6 \text{ hrs}\\
& = 20 \text{ gal} - 0.93 \text{ gal}\\
& = 19.07\\
& \approx 19.0.
\end{align*}