On Mon, 2010-08-23 at 23:16 -0600, Ron Jensen wrote:
> On Monday 23 August 2010 21:37:06 Ampere K. wrote:
>
> > Thank you very much Jon and Ron. That certainly cleared things up for me.
>
> You're welcome
>
> > I only have one question left, which is my original question regarding
> > turbofan
> Now I am getting confused. I need an example.
>
> Say if I have the following entry:
>
> Drag_at_zero_lift
>
> aero/qbar-psf
> metrics/Sw-sqft
> 0.016
>
>
>
>
] Extracting stability derivatives in JSBsim/Yasim
Hello all,
How would I go about extracting the stability derivatives from the FDM in
JSBsim and Yasim? I would also like to extract the stability derivatives from
the engine model.
Ampere
> Hello Jon,
>
> I found table entries such as "aero/coefficient/CDalpha". I'm guessing
> those are the non-dimensional derivatives?
Ampere,
The property names starting with "aero/coefficient" are actually misleading.
Historically, they really were coefficients. Now, however, the functions in
t
On August 19, 2010 08:32:50 pm Jon S. Berndt wrote:
>
> Look at the aircraft config file. The functions in that section define
> forces and moments. If you know the non-dimensionalizing parameters, you
> can extract the derivatives.
>
> What is it that you need from the engine?
>
> Jon
Hello J
> Hello all,
>
> How would I go about extracting the stability derivatives from the FDM
> in
> JSBsim and Yasim? I would also like to extract the stability
> derivatives from
> the engine model.
>
>
> Ampere
Look at the aircraft config file. The functions in that section define
forces and mome
Hello all,
How would I go about extracting the stability derivatives from the FDM in
JSBsim and Yasim? I would also like to extract the stability derivatives from
the engine model.
Ampere
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