On September 25, 2008 01:43:31 am Ampere K. wrote:
> eq(A) dt =
> [1, -d psi, d theta; d psi, 1, -d phi; -d theta, d psi, 1][phi; theta; psi]
> - [1, 0, 0; 0 1 0; 0 0 1][phi; theta; psi]
Whoops. I meant:
eq(A) dt =
[1, -d psi, d theta; d psi, 1, -d phi; -d theta, d psi, 1] -
[1, 0, 0; 0 1 0;
Thanks for the reply. I've just looked through that section, and it seem that
omega x v
(eq. 1.5-13)
is a recurring theme in dynamics modelling. After doing unit analysis, I
found that it gives acceleration. So I guess I will try making use of it in
my own equations of motion.
Another thing
: FlightGear developers discussions
> Subject: [Flightgear-devel] Questions on flight model
>
> Hello all,
>
> As part of a project at school, I have been trying to come up with
> equations
> of motion for an aerial platform, so that I may use the equations to
> design a
Hello all,
As part of a project at school, I have been trying to come up with equations
of motion for an aerial platform, so that I may use the equations to design a
control system. The issue is that I'm having trouble coupling linear and
angular dynamics. Specifically, I need to describe the
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