I agree that - at least - we should mention it in the documentation. We could  
hypothetically also accept data in any of the supported frames. Unfortunately, 
a lot of the data present in technical reports (NACA/NASA/AIAA) that I have 
seen is ambiguous as to frame for the rotational coefficients. When I get aero 
data it has usually already been reduced by the supplier. I do recall seeing 
aero data being supplied in stability frame, once. By default, we'll always 
assume rotational coefficients are expressed in body frame. We will think about 
adding support for other frames, but another thing I've done is to do the 
conversion inline as a function in the aerodynamics element.

Jon

----- Reply message -----
From: "Alan Teeder" <ajtee...@v-twin.org.uk>
To: "FlightGear developers discussions" <flightgear-devel@lists.sourceforge.net>
Cc: "issues Development" <jsbsim-de...@lists.sourceforge.net>
Subject: [Jsbsim-devel] [Flightgear-devel] about fdm properties
Date: Sat, May 11, 2013 9:28 AM


The problem is that it is not documented that JSBSim only accepts body axis 
derivatives/aero coefficients for the rotary axes. The linear axis has the 
choice of body or wind/stability axes. I had assumed (wrongly) that as it 
was not specified, the rotary axes used the same axis frame as the linear 
axes. The result was an aircraft that was unaccountably  uncontrollable at 
high angles of attack.

By posting here I was trying to bring this matter to Flightgear developers 
attention. I cross posted the same message to JSBSim and Datcom mailing 
lists.

Jon Berndt has replied on the JSBSim list saying "I don't recall seeing a 
set of rotational coefficients given in stability or wind frame." 
Unfortunately this is far from being the case.

In my working life running the research simulator at BAC Weybridge the only 
body axis data that I can recall being given was for the Concorde, back in 
1968/9. All other aircraft that I worked on used wind axis data.   Datcom is 
of particular relevance to JSBSim FDM authors and gives its output in 
stability axes.

Perhaps I should add this to the JSBSim bug list 
http://sourceforge.net/p/jsbsim/bugs/, but this still has open bugs from 
2003/4.

What is needed is at minimum is a documentation update. However, due to the 
number of Datcom based FDMs, it would be better to add full support for 
stability axes.

I have cross-posted this to the JSBSim list.

Alan




-----Original Message----- 
From: Anders Gidenstam
Sent: Saturday, May 11, 2013 3:41 PM
To: FlightGear developers discussions
Subject: Re: [Flightgear-devel] about fdm properties

On Fri, 3 May 2013, Alan Teeder wrote:

> It exposes a serious problem in JSBSim which affects all Datcom users.

Isn't it rather a missing feature than a fault in JSBSim?

The JSBSim documentation and axis names are fairly clear on that the
moments are specified around the yaw, pitch and roll axes (but the origin
is at AeroRP rather than at the body frame origin/CoG so additional
corrections according to the parallel axis theorem are added based on the
distance from AeroRP to the actual CoG).

If the DATCOM -> JSBSim input translation is faulty (I have no
professional grounding in aerodynamics and I cannot tell) the best place
to get it addressed might be at the mailing list/group for Bill
Galbraith's DATCOM+ program (I think it is the most commonly used way
to generate a JSBSim configuration from DATCOM):

http://tech.groups.yahoo.com/group/digital_datcom/

Cheers,

Anders
-- 
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