Beagle Pup experiment

Everything in connection with developing aircraft for FlightGear
Richard
Posts: 114
Joined: Sun Sep 11, 2016 5:57 pm

Re: Beagle Pup experiment

Postby Richard » Fri Nov 25, 2016 9:38 pm

I've also figured out how to use OpenVSP to calculate the moments of interia; this will probably be better than Simon's method where you define the positions and mass and let JSBSim figure it out, simply because JSBSim makes assumptions about the size of the masses. VSPAero will take slices through the model and based on the density you assign will calculate the mass and inertias. I've added a section to my writeup (http://chateau-logic.com/content/using- ... flightgear) that covers this.

So here is a new version of my FDM with fixed instability, fixed moments of inertia and revised geometry. http://chateau-logic.com/sites/default/ ... 6-11-25.7z

I shall now go and fly sanhozay's new fdm and see how it compares

sanhozay
Posts: 167
Joined: Fri Sep 25, 2015 5:59 pm

Re: Beagle Pup experiment

Postby sanhozay » Fri Nov 25, 2016 9:58 pm

Richard wrote:Wing incidence I now have at 0; but adjusted the tail to 1.9 (leading edge down) take this into account for stability purposes however it's not going to be quite right - I did it like this after getting very confused about whether or not I needed to use wing alpha or FRL alpha for the coefficient base of all of the surfaces. I spent about 7 evenings tuning this to get the right pitching moment.

Interesting. I fudged mine with elevator trim, which is not a long term solution but I needed it to make it glide and to avoid the nose pitching down during the takeoff roll. Default Aeromatic ignores wing incidence I believe, and something I was going to try was use alpha-wing-rad in place of alpha-rad.

Your new inertias:

Code: Select all

Ixx   Iyy   Izz   Ixy   Ixz   Iyz               
549.91   636.08   1145.26   0.00   17.29   0.08      

My inertias estimated by Aeromatic++:

Code: Select all

 <ixx unit="SLUG*FT2">    589.07 </ixx>
    <iyy unit="SLUG*FT2">    572.46 </iyy>
    <izz unit="SLUG*FT2">   1078.08 </izz>

What units are you CoG numbers? Feet? And where's the datum?

Richard
Posts: 114
Joined: Sun Sep 11, 2016 5:57 pm

Re: Beagle Pup experiment

Postby Richard » Fri Nov 25, 2016 11:21 pm

Interesting that our inertias are close; that's a testament to the new Aeromatic, (and maybe the old one). I've spent a lot of time trying to figure out how to calculate MOI over the last few weeks - I've always understood the calculation of MOI to be a bit of a black art practised by skilled slide rule practitioners in darkened rooms with nary a glimpse at a computer (I'm probably very wrong about this).

All my dimensions are in feet. For VSPAERO the latest run was using AERORP of 6.8,0,0 - however as part of my pitch moment tuning I've had everything from 8.2 to 5.2; from the Beagle figures below 6.8 is close to the aft limit (assuming all my other measurements are right which is unlikely), so the 6.8 is really the result of tuning to get the right sort of stability and basic pitch moment curve..

Using the usual 25% MAC I came up with a CoG range from 6.4981, 6.9211 - using a wing root X of 5.779 and a MAC of 4.23

Beagle themselves refer to an older way of expressing this (SMC); when they state (aft CG limit of 27.5% SMC) (S/b) - which gives us a range of 6.39 to 6.83 (feet);

I've just been flying your revised FDM and it's definitely an improvement. You should be using a kinematic for the control surfaces as they snap to position as they're directly linked to the input device positions - and whilst most of the time with a joystick you won't notice this it is noticeable when using the keyboard (centre all controls NUMPAD 5) or mouse. I think the controls on the craft are connected directly by wire so a 0.2 second kinematic would probably be a good point to get controls that move as though they are connected to things with mass and resistance.

It all goes horribly wrong though if I have maximum deflection (stick back) on the elevators; at 30 degrees of pitch the model becomes numerically unstable. During the takeoff roll I had a lot of trouble controlling the yaw using the rudder but managed to get airborne on my second attempt.

In flight it feels much too responsive; almost massless with no inertia (which I know isn't true because I've seen your inertias and they are the same as mine); so maybe it's the p,q,r damping that isn't right.

bomber
Posts: 1379
Joined: Mon Nov 30, 2015 3:40 pm

Re: Beagle Pup experiment

Postby bomber » Fri Nov 25, 2016 11:27 pm

This is genuinely so much fun. .....thank you guys for taking part.
"If anyone ever tells you anything about an aeroplane which is so bloody complicated you can't understand it, take it from me - it's all balls" - R J Mitchell

sanhozay
Posts: 167
Joined: Fri Sep 25, 2015 5:59 pm

Re: Beagle Pup experiment

Postby sanhozay » Sat Nov 26, 2016 8:25 am

Thanks for your advice regarding the kinematics. I never fly with the keyboard so I wouldn't have noticed.

Richard wrote:In flight it feels much too responsive; almost massless with no inertia (which I know isn't true because I've seen your inertias and they are the same as mine); so maybe it's the p,q,r damping that isn't right.

I'm surprised by this. Compared to my previous model it's much less responsive. I thought it felt on the stiff side compared to other Flightgear models but I'm wary of making such feel judgements as I've never even set eyes on a Beagle Pup, let alone flown one.

If you feel like playing with them, there are tuning coefficients under fdm/tuning for pitch, roll and yaw damping. They are set to 1.0 to use the Aeromatic defaults and simply scale the pitch/roll/yaw moment due to pitch/roll/yaw rate elements.

User avatar
IAHM-COL
Posts: 6455
Joined: Sat Sep 12, 2015 3:43 pm
Location: Homey, NV (KXTA) - U.S.A
Contact:

Re: Beagle Pup experiment

Postby IAHM-COL » Sun Nov 27, 2016 3:57 am

sanhozay wrote:@IAHM-COL: When I've finished tuning, I was hoping you'd test the 11,700ft service ceiling by taking it to Innsbruck.

Getting out would probably be more interesting than getting in. :lol:


T'is the track

http://mpserver15.flightgear.org/modules/fgtracker/?FUNCT=FLIGHT&FLIGHTID=6843083

Flies nice :D
https://raw.githubusercontent.com/IAHM-COL/gpg-pubkey/master/pubkey.asc

R.M.S.
If we gave everybody in the World free software today, but we failed to teach them about the four freedoms, five years from now, would they still have it?

sanhozay
Posts: 167
Joined: Fri Sep 25, 2015 5:59 pm

Re: Beagle Pup experiment

Postby sanhozay » Sun Nov 27, 2016 11:05 am

You went that way out of Innsbruck on a 100hp engine! :shock: :lol:

Thanks for testing. So about 25 minutes to get to 10,000 from 1,900 and 40 minutes to get up to service ceiling. That's in the right ballpark. When I have a half hour to waste, I'll log a climb from s/l to 10,000 (which should be ~31 minutes).

User avatar
IAHM-COL
Posts: 6455
Joined: Sat Sep 12, 2015 3:43 pm
Location: Homey, NV (KXTA) - U.S.A
Contact:

Re: Beagle Pup experiment

Postby IAHM-COL » Sun Nov 27, 2016 3:58 pm

I had good luck.
I had marginal VFR till about 8000, so I could just rollercoasted the mountain side visually. When I reached 8000 feet the weather changed to overcast at low altitudes and I began flyin a haze, so I switched to VFR and kept 11700 for cruising :P
https://raw.githubusercontent.com/IAHM-COL/gpg-pubkey/master/pubkey.asc

R.M.S.
If we gave everybody in the World free software today, but we failed to teach them about the four freedoms, five years from now, would they still have it?

bomber
Posts: 1379
Joined: Mon Nov 30, 2015 3:40 pm

Re: Beagle Pup experiment

Postby bomber » Sun Nov 27, 2016 3:58 pm

Update on the way.... hopefully I've not forgotten anything...

I've added an engine system file to reduce the Ve at low throttle and something for the start-up to look a little less like you're throwing the switch on an electric motor.

Also I've included this time my working documents, so you have my spreadsheets and drawings plus url links to web based data.
"If anyone ever tells you anything about an aeroplane which is so bloody complicated you can't understand it, take it from me - it's all balls" - R J Mitchell

User avatar
IAHM-COL
Posts: 6455
Joined: Sat Sep 12, 2015 3:43 pm
Location: Homey, NV (KXTA) - U.S.A
Contact:

Re: Beagle Pup experiment

Postby IAHM-COL » Sun Nov 27, 2016 4:06 pm

anytime you ready shoot me the email, and I push
https://raw.githubusercontent.com/IAHM-COL/gpg-pubkey/master/pubkey.asc

R.M.S.
If we gave everybody in the World free software today, but we failed to teach them about the four freedoms, five years from now, would they still have it?


Return to “Aircraft Development”

Who is online

Users browsing this forum: No registered users and 99 guests