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Model of Airplane Descent Path to Landing

Using the graph of a Boeing 787's descent path to landing, create a mathematical model of the path.
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Set up the GLSP

Airplane landings typically follow a smooth curve. A linear line would be too sharp. A quadratic path would cause us to crash. However, a cubic polynomial seems to provide a smooth curve, which we will use to model the descent.

p(x)=a0+a1x+a2x2+a3x3

Our goal is to find the parameters a0,a1,a2,a3 that fit the path of our Boeing 787. To determine the unknown coefficients, we impose the following conditions.

Condition #Verbal DescriptionEquation1.The cruising altitude is 40000 ftp(0)=40000at the start of the descent.2.The landing point has an altitudep(400)=0of 0.3.The tangent line to the descentp(0)=0path is horizontal at the start.4.The tangent line to the descentp(400)=0path is horizontal at the landing.

Let's take a look at what each condition means.

Condition 1

We start our landing process at 40000 ft in the air and we assume this is 0 miles. In other words, we begin with our first equation p(0)=40000. By substituting in x=0 and p(0)=400000, we see

1a0+0a1+0a2+0a3=40000

This is a linear equation based on the fact that we know the input and know the output. We can rewrite this as an 5.1 Inner Product Between Vectors.

[1000][a0a1a2a3]=40000

Condition 2

We also know that our altitude will be 0 when we land. From our graph, we see that the altitude reaches 0 when x is 400 miles. Plugging x=400 and p(400)=0 into our cubic polynomial, we see

1a0+400a1+4002a2+4003a3=0

Once again, we can write this linear equation as an inner product.

[140040024003][a0a1a2a3]=0

Recall that matrices and vectors are data structures used to help us organize data. We can arrange our equations from conditions 1 and 2 into row form to produce 17.1 The General Linear-Systems Problem.

[1000140040024003]2×4[a0a1a2a3]4×1=[400000]2×1

When we have a short and wide matrix, we generally have too many (infinite!) possible solutions. We need to enforce more constraints to produce a meaningful solution.

Condition 3

Before landing, we want our plane to be traveling horizontally. Mathematically, we can say we want the tangent line of our path to have 0 slope at the moment it starts to descend. Written using mathematical notation, we see

p(0)=0

We can also take the derivative of our function p(x).

p(x)=a0+a1x+a2x2+a3x3p(x)=a1+2a2x+3a3x2

When we substitute in x=0 and p(0)=0, we get at third equation.

0a0+1a1+20a2+302a3=0

Once again, we can write this equation as an inner product.

[0100][a0a1a2a3]=0

This is now a third condition we can put into a matrix.

Condition 4

We also want the tangent line at the end of the landing path to have a 0 slope. After all, we do not want to crash into the ground.

p(400)=0

We can plug this value into our equation for p(x).

0a0+400a1+2400a2+34002a3=00a0+1a1+800a2+480000a3=0

And written as an inner product we see

[01800480000][a0a1a2a3]=0

Combining Conditions

Let's combine all four of these equations into a single system.

1a0+0a1+0a2+0a3=400001a0+400a1+160000a2+64000000a3=00a0+1a1+0a2+0a3=00a0+1a1+800a2+480000a3=0

Each equation can be stored as a product. We can organize these products using matrices to form the system.

[1000140016000064000000010001800480000]A[a0a1a2a3]x=[40000000]b

We have successfully set up a general linear-systems problem from a real world context. See 17.5 Solving GLSP for Airplane Descent Path for the final solution to this modeling problem.