I'm currently studying Stability of Flight, and there's a topic in this course that treats aircraft responses to certain maneuvers of the pilot.
Consider for example, the impulsive deflection of the rudder of an airplane, so that the angle of the deflection in time is given by:
\begin{equation} \delta_r(t)=% \begin{cases} \delta_r &\text{if $t=0$}\\ 0 &\text{if $t\neq 0$}. \end{cases} \hspace{15pt}(1) \end{equation}
where $\delta_r$ is a constant.
[Note: This is an approximation of the real input. In reality the input is a continuous function, with a big variation (until $\delta_r$) on the instant of the action.]
Normally this type of action is expressed as:
$$\delta_r(t)=\delta_r\delta(t)\hspace{15pt}(2)$$
where $\delta(t)$ is the Dirac delta function. My problem is that these two expressions aren't equivalent, because the Dirac delta function is a distribution so that:
\begin{equation} \delta(t)=% \begin{cases} \infty &\text{if $t=0$}\\ 0 &\text{if $t\neq 0$}. \end{cases} \hspace{15pt} (3) \end{equation}
[Note: I know that this is also an approximation. Dirac delta function is a continuos function that tends to infinity in the instant of the action.]
So the expression (2) can only express the density of the action in time. To $(1)$ and $(2)$ be equivalent, the $\infty$ in (3) should be 1. I've seen this consideration in others areas of science, for example on Electronics, an applied impulsive voltage on a circuit is expressed in the same way as the deflection of the rudder of the airplane.
I think that a good model of an impulse input should have the same behavior of the Dirac delta, but with a normalization to 1. Am I missing something?