Consider the following problem. We have a set of 21 data points,
representing measurements of a rocket altitude during flight at 21
consecutive time moments. We know that, in an uniformly accelerated motion,
the altitude as a function of time is given by
t h(t) t h(t) t h(t) ------------ ------------ ------------ 0.0 -0.2173 0.7 3.3365 1.4 6.3312 0.1 1.0788 0.8 1.9122 1.5 6.3549 0.2 0.1517 0.9 3.0594 1.6 8.5257 0.3 0.1307 1.0 3.7376 1.7 8.7116 0.4 1.4589 1.1 3.3068 1.8 8.2902 0.5 2.9535 1.2 3.7606 1.9 11.4596 0.6 2.4486 1.3 6.6112 2.0 11.2895we try to infer the parameters , , , which define the smooth curve (). In particular, the acceleration of the vehicle is , and, if is the mass of the rocket and is the gravitational acceleration, then we can infer the total force produced by thrusters .
Note that we have 21 data points to determine 3 parameters; the data is corrupted by measurement errors (for example, the first altitude is negative!). We will use the redundancy in the data to ``smooth out'' these measurement errors; see Figure for the distribution of data points and the parametrized curve.
At each time moment , we are given the measured height
(in the data set); the height obtained by the formula ()
is
. Therefore, the formula ()
``approximates'' the measured height at time with an error
We want the values , and chosen such that the
differences between the model and the measurements
are small. Therefore, we impose that
the sum of squares of errors is minimized