Aircraft System Identification: Theory and Practice

In the context of system identification applied to aircraft, regression refers to a statistical technique for modeling and investigating relationships among measured variables. An example of a regression is the following model relating the nondimensional pitching moment coefficient C m, to angle of attack ? and Mach number M, for data collected during a wind-tunnel test:
In this example, ? and M are variables that are set to selected values for each experimental test point, and measurements of ?, M, and C m are made. The pitching moment coefficient C m is assumed to depend on ? and M in the manner postulated by the form of the model shown in Eq. (5.1), where
,
,
, and
are constant model parameters to be determined. Accordingly, ? and M are called the independent variables, and C m is called the dependent variable or the response variable. There may be other variables that could affect C m, but these are held fixed during the test, insofar as it is known what the influential variables might be.
Since the independent variables ? and M are set by the experimenter for each data point, it is assumed that they can be measured without error. The dependent variable C m is subject to random measurement errors, and is therefore a random variable. The random error term v m includes random effects of unknown...