CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).

Patrick, Mon Mar 26 2012, 03:53AM

CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3.)



Supporting threads:

Link2 CSU Chico Tilt Rotor Flying Machine, (Programming and CPU, 3 of 3).



PDF's: (soon)
gyro
accerl
mag
stm32's
IR proximity sensors.
U-dar



YouTube:
Link2 Avatar Scorpion Gunship RC - TwinCopter



Related threads:
Differences between good fiberglass, and good Carbon fiber. Link2
International Aerial Robotics Competition, Mission 6, 2011. Link2
69mm Electric Ducted Fan, 2.8 lbs Static Thrust... Link2
Need help with the STM32F4-Discovery board... Link2



Pics!

1332738654 2431 FT1630 Sam 1312
please forgive the paper plates, i needed to show the fan placement, but they're not ready yet.


1332738654 2431 FT1630 Sam 1314



1332741180 2431 FT1630 Sam 1326
Titanium gear digital servo.



1332742397 2431 FT1630 Similar
A similar metal gear servo.



1332730999 2431 FT1630 Sam 1310
Its got guts!!!


1332734000 2431 FT0 Sam 1308
37 inches long in this pic. No motors or rotors yet.


1333074657 2431 FT1630 Sam 1326a



1333074657 2431 FT1630 Sam 1319


Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Carbon_Rod, Mon Mar 26 2012, 05:44AM

Do you plan to cut holes in the air frame to fit the battery and servos?

Note, loose cable ties and Styrofoam often help PCB survive torsional strains during impact.
It would be wise to anchor the main ESC battery connection cable to the air frame so it will pull-free from the battery during impact.... wink


The Oak and the Reed, Jean de la Fontaine (1621-1695)

The Oak spoke one day to the Reed
"You have good reason to complain;
A Wren for you is a load indeed;
The smallest wind bends you in twain.
You are forced to bend your head;
While my crown faces the plains
And not content to block the sun
Braves the efforts of the rains.
What for you is a North Wind is for me but a zephyr.
Were you to grow within my shade
Which covers the whole neighbourhood
You'd have no reason to be afraid
For I would keep you from the storm.
Instead you usually grow
In places humid, where the winds doth blow.
Nature to thee hath been unkind."
"Your compassion", replied the Reed
"Shows a noble character indeed;
But do not worry: the winds for me
Are much less dangerous than for thee;
I bend, not break. You have 'til now
Resisted their great force unbowed,
But beware.
As he said these very words
A violent angry storm arose.
The tree held strong; the Reed he bent.
The wind redoubled and did not relent,
Until finally it uprooted the poor Oak
Whose head had been in the heavens
And roots among the dead folk.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Mon Mar 26 2012, 06:19AM

Yep, ill be using holes, and a battery tray to secure stuff. i would rather bend something than have it break off.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Dago, Mon Mar 26 2012, 08:13AM

Heh that looks neat. Kinda like a segway except it flies.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Mon Mar 26 2012, 08:29AM

Maybe I'm missing something, but it looks like the centre of gravity will be a long way away from the centre of lift, especially once you've added the battery pack.

Link2

In the above picture of a Boeing Osprey, the rotors are roughly in the middle of the aircraft.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Mon Mar 26 2012, 02:00PM

Steve Conner wrote ...

Maybe I'm missing something, but it looks like the centre of gravity will be a long way away from the centre of lift, especially once you've added the battery pack.

Link2

In the above picture of a Boeing Osprey, the rotors are roughly in the middle of the aircraft.
my CG, CL, and CP will all be approximately centered in between the rotors (as in the V-22), the tail only looks heavy its pretty light, and the sensors (MS kinnect and U-dar) are pretty heavy they go in front (with the battery). so it all balances out. its all very Zen.


Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Mar 28 2012, 06:52AM

Airframe whieghs 631 grams. (too much!)
servo and torque tube arrangement wheighs 272 g.
ESC's w/wire wheigh 142 g
11.1v 2200mAh battery wheighs 190 g.
circuit boards 65 g.

-----------------------------------------------
total mass is about 1.490 Kg's.

i need to lighten the airframe by about 300 grams.



Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Wed Mar 28 2012, 09:19AM

Well, what is the tail there for? It can't be for aerodynamic stability. If your design needed the tail for stability, it would be unstable in hover mode, when there's no airflow over it. So I suggest chopping it off. tongue

The Osprey (and its RC model version from Rotormast) needs helicopter-style rotors with cyclic pitch control. These can generate a pitching moment to control the vehicle in the pitch axis. A quadrotor does that by having rotors fore and aft of the CG.

You don't seem to have any active control in the pitch axis at all. No matter how you tilt your rotors, the thrust vector will always pass through the CG and there'll be no pitching moment.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Mar 28 2012, 01:51PM

Steve Conner wrote ...

Well, what is the tail there for? It can't be for aerodynamic stability. If your design needed the tail for stability, it would be unstable in hover mode, when there's no airflow over it. So I suggest chopping it off. tongue

The Osprey (and its RC model version from Rotormast) needs helicopter-style rotors with cyclic pitch control. These can generate a pitching moment to control the vehicle in the pitch axis. A quadrotor does that by having rotors fore and aft of the CG.

You don't seem to have any active control in the pitch axis at all. No matter how you tilt your rotors, the thrust vector will always pass through the CG and there'll be no pitching moment. If you look at the you tube clip link above youll see his "twin copter " remain quite usable even when manuevered flat. pitching and rolling seemed to cause problems in narrow office hallways when i was at IARC 2011. for that reason i wanted to use yaw and tilt instead.


yepp as soon as i dont need the magnetometer ill be chopping the tail off (it was mostly for crash protection, and to look spiffy), also i used to much epoxy on one side on the FG. my gaol is to get the total airframe down to 250 grams or less.

As for the pitch and CG comment, i see no problem, i want the sensor plane (the airframe) to remain flat even when the rotors are full forward or aft. the last thing i want is my sensor plane rotating as im trying to update the SLAM model.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Thu Mar 29 2012, 07:33AM

OK, but my point is: Let's say your vehicle acquires a pitch error. Maybe a gust of wind tips the nose up. How will the control system correct it?
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Thu Mar 29 2012, 09:02PM

Steve Conner wrote ...

OK, but my point is: Let's say your vehicle acquires a pitch error. Maybe a gust of wind tips the nose up. How will the control system correct it?
I fail to see why tilting both rotor fans to counter the unwannted pitch up, wont work. isnt this what the v-22 does? or does the V-22 use variable pitch to increase effective collective.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Fri Mar 30 2012, 07:19AM

Well, the problem is: If you made the thrust vector of the fans pass through the centre of gravity, then there won't be any pitching moment no matter how you tilt them. And if you didn't, then you'll have other serious stability problems. Either it won't hover or it won't convert.

I don't know for sure, but I guess the V22's rotors both have cyclic pitch control like a helicopter. The blades vary pitch in time with the rotation, allowing the thrust vector to be placed anywhere you want.

For example, if a helicopter wants to move forward: The cyclic pitch control causes the rear half of the rotor to produce more thrust than the front. This moves the thrust vector aft of the CG, causing the nose to pitch down. The thrust vector now has a component rearwards as well as downwards, and the chopper moves forward.

A multicopter works in exactly the same way, modulating power to its four small rotors to move the thrust vector around as required. Except with only two fans, you can't move it fore and aft.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Electroholic, Fri Mar 30 2012, 01:03PM

I think if the CoG hangs below the tilting axis, then everything works.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Fri Mar 30 2012, 03:44PM

Electroholic wrote ...

I think if the CoG hangs below the tilting axis, then everything works.
yeah i think so, then its like a pendulum, and i think it becomes a first order stability problem. I think. I noticed a slight dihedral on the kkmulticopter's fans in that video. That (and having the CoG low) should give some restoring force to large scale stability (favoring controlability) , while still allowing small signal instability (Still allowing maneuverability).



Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Mon Apr 16 2012, 10:47PM

ok CF and GF are cut out and curing, progress so far:



1334616436 2431 FT136218 Sam 1363
Seen here the dry layers,

3 layers of FG, plain weave, 73 grams dry. Quasiisotopic, should be about 0.030" thick.
5 layers of CF, 2x2 twill weave, 156 grams dry. Quasiisiotropic, should be about .055" thick.

total dry wheight is 229 grams. untrimmed.

Now we see if im talented enuff to screw it all up by adding to much epoxy!



Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Apr 18 2012, 03:52AM

it weighs in at 400 grams, + a few mods im adding, but subtracting their weight from my other budget mass items.so its all going well. Its super strong and light. only a few pultruded peices and balsa need to be added.


1334721136 2431 FT136218 Sam 1375
Seen here curing, then it will be sheared down to the white line. Next time ill use 4 layers of CF instead of 5, and then embed the balsa between two layer of two CF, still being quasiisotropic.What you see is the Gen 2 airframe.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Mon Apr 23 2012, 11:06PM

Ive got this forum posting. which raises the issues already discussed on our threads here.

Link2 tilt rotor, RC forums.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Sun May 06 2012, 06:11AM

Weights:

MS Kinect : 144 g
Airframe w/o Tail : 197 g
4 cell lipo: 250 g
Left Wing : 320 g
Right wing : 320 g
main boards : 60 g
ESC's w/ reciever : 170 g
Gyros, accel's : 40 g
servo tray : 120 g
------------------------------
total mass : 1,621 g



Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Tue Jun 12 2012, 10:20PM

IT WORKS!!!

it does fly, however, its unstable in the pitch axis. (As someone predicted [Steve Connor]) i will try to increase the vertical moment arm from 1.2 inches, to about 3 inches. Hopefully that will give gravity more influence on the pitch.

i would like to be able to calculate things out, instead of guessing. But at the moment the measurements, math, and physics elude me...

I have video and many pics, but ive got to edit it all down to reasonable file types and sizes...more posts to come!


1339539652 2431 FT136218 Sam 1459

1339539652 2431 FT136218 Sam 1455

1339539652 2431 FT136218 Sam 1386
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Wed Jun 13 2012, 01:57AM

Patrick wrote ...

it does fly, however, its unstable in the pitch axis. (As someone predicted [Steve Connor]) i will try to increase the vertical moment arm from 1.2 inches, to about 3 inches. Hopefully that will give gravity more influence on the pitch.

I think you are still failing to understand Steve's comment.

Have you tried drawing a force diagram? I am interested to see if you can locate the restoring moment you assume exists.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jun 13 2012, 03:01AM

AndrewM wrote ...


I think you are still failing to understand Steve's comment.

Have you tried drawing a force diagram? I am interested to see if you can locate the restoring moment you assume exists.

I realize i maynot have a full grasp on the statics or dynamics at hand, but lengthening the vertical moment arm did have a profound efffect on pitch and stability... it not perfect and 3 inches, but its flyable and manageble..

ill will draw a free body diagram as soon as i figure it out, but i want some evaluation from others on the situation.

im totally exhausted, ready for bed...
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Wed Jun 13 2012, 04:05AM

Patrick wrote ...

AndrewM wrote ...


I think you are still failing to understand Steve's comment.

Have you tried drawing a force diagram? I am interested to see if you can locate the restoring moment you assume exists.

I realize i maynot have a full grasp on the statics or dynamics at hand, but lengthening the vertical moment arm did have a profound efffect on pitch and stability... it not perfect and 3 inches, but its flyable and manageble..

ill will draw a free body diagram as soon as i figure it out, but i want some evaluation from others on the situation.

im totally exhausted, ready for bed...

Well I'll just give you the answer - increasing the arm length increased your moment of inertia (by a factor of 4) so your instability just progressed 4x slower. But there is no possible "pendulum" effect in your system.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jun 13 2012, 04:09AM

AndrewM wrote ...


Well I'll just give you the answer - increasing the arm length increased your moment of inertia (by a factor of 4) so your instability just progressed 4x slower. But there is no possible "pendulum" effect in your system.

ok, but that gives my gyros and PID loops time to put the commands on the servos, and gives the mechanical train time to alter the forces, right?

after all it can be made to work... Link2


Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Wed Jun 13 2012, 05:27AM

Absolutely, lots of the flying toys you see now are statically unstable. Active control makes short work of the issue provided you have enough inertia to give it time to react.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jun 13 2012, 06:16AM

Ok so i was wrong about the reasoning (the pendulum) but i was right that increasing the distance bewtween the CL and CG that the time of instability is longer? right?
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Wed Jun 13 2012, 06:19AM

Well, congrats on getting it to fly! smile
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jun 13 2012, 06:38AM

Steve Conner wrote ...

Well, congrats on getting it to fly! smile
yeah and as unstable as it is, we only broke one of the cheap servos... so now its will soon be time for the Savox servos and good 11" props! i just need to make it more stable.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Carbon_Rod, Wed Jun 13 2012, 08:32AM

Note attaching a balanced wooden stick on a hinge to the airframe with string will provide a "safe" platform for calibration (or finding cg). Without this simple rig people tend to chew through more props etc.

Out of all the sensors, you will likely find a good 3-axis compass provides cleaner data.
However, large metal beams/cars will cause interference (most GPS units also suffer precision loss in urban settings).

Cheers,
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Wed Jun 13 2012, 02:38PM

Patrick wrote ...

Ok so i was wrong about the reasoning (the pendulum) but i was right that increasing the distance bewtween the CL and CG that the time of instability is longer? right?

Yep.


Carbon_Rod wrote ...

Note attaching a balanced wooden stick on a hinge to the airframe with string will provide a "safe" platform for calibration (or finding cg). Without this simple rig people tend to chew through more props etc.

This idea also reminded me - you might consider attaching a number of 4' long wooden sticks to your models primary axes. These will greatly increase your moments of inertia while adding fairly little mass. It will be much easier to fly and tune.

An example is these popular coaxial helicopters:
250

There is, in fact, nothing inside that fail boom; its just a thin plastic shell. However its not purely decorative; without that boom it is completely unflyable as the gyro and control loop cannot damp the oscillations.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Josh Campbell, Wed Jun 13 2012, 03:45PM

Can't wait to see some videos of this design in action! (Maybe YouTube so file size would not be an issue...) Congrats on getting it to fly. :)
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jun 13 2012, 05:41PM

AndrewM wrote ...


This idea also reminded me - you might consider attaching a number of 4' long wooden sticks to your models primary axes. These will greatly increase your moments of inertia while adding fairly little mass. It will be much easier to fly and tune.

An example is these popular coaxial helicopters:
250

There is, in fact, nothing inside that fail boom; its just a thin plastic shell. However its not purely decorative; without that boom it is completely unflyable as the gyro and control loop cannot damp the oscillations.

thats a great idea, ill do that and report back!


EDIT: ill only put one rod on the roll axis, thats the only axis thats really problematic.

EDIT: It worked... Duh! now i see what steve and andrewM meant, when i lifted the CL above the CG i was creating a vertical pseudo-rod, which helped the pitch some what. As for roll, the rod worked perfectly, even the high freq oscillations in RPM are gone. it's like flying a wholly different machine now!!! Both my ace pilot Corey Koehler and I can fly it...he better than I, but with accerlometers i can definatly program a waypoint and computer pilot, and then generate a SLAM model in real time.

AI flight and IARC 2012 are now within my grasp.

Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Thu Jun 14 2012, 03:33PM

Ok here are the modified pics of the airframe...


1339687984 2431 FT136218 Sam 1508
48" long wood rod with steel washers.


1339687984 2431 FT136218 Sam 1506
Torque tube and Power 10 motor.


1339687984 2431 FT136218 Sam 1499
Servo and Fan section.


1339687984 2431 FT136218 Sam 1498
All up machine.

Im still trying to figure out video, so give me awhile. I dont want to kill the sites storage...
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Thu Jun 14 2012, 09:33PM

I think the easiest way to post video on here is: upload it to noobtube, make it unlisted so regular Youtube users can't view or comment on it, and allow embedding. Then use the YouTube button in the forum editor to add a link to it, and the video will appear right in the thread.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Fri Jun 15 2012, 06:35AM

Im still trying to figure out video clips so please excuse the breif lame clip below, ill also trying to get a YouToob channel up soon.


CSU Chico Flight Club, Tilt Rotor UAV for IARC 2012.

Description: "Tilt Rotor UAV Drone Test, CSU Chico Flight Club. Flight test conducted by Corey Koehler (A Main Hobbies.com) and Patrick Coleman (EE, CSU Chico), seen in the above clip is the dreaded roll oscillation. This problem has since been solved."

This clip shows the rapid oscillations in the roll axis (left and right tweaking out), then we land it, as of now the rod suggested by AndrewM, has solved this problem entirely.

EDIT: I think this is my YouTube channel, is it? Link2

I dont know how to put text bubbles pointing to places in the video, which for tecnichal demonstrations is kind of important.



Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Sat Jun 16 2012, 04:58AM

New pics of servo horns...


1339822716 2431 FT136218 Sam 1513a
Old horn on top, new horn being made on bottom.


1339822716 2431 FT136218 Sam 1514a
Broke a tap, consequently i have started drinking tonight...


1339822716 2431 FT136218 Sam 1517a
Notice the recessed nut hole for the ball stud.


1339822716 2431 FT136218 Sam 1519a
Ball socket turnbuckle, made from hardened titanium, 2.350 inches long.

Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Tue Jun 26 2012, 01:50AM

oops! crashed it!!

it works well, CG, CR, CL have all been balanced and tuned to the point where it holds a hover, however its still difficult for me to fly. And i crashed it in, broke a titanium gear. Anyway i still need to generate a velocity PID controller to operate from data provided from the 9 DOF gyro-mag-accel MEMS IMU....
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jun 27 2012, 02:06AM

Ok having evaluated the recent crash and damage, i believe it is vulnerable to "pitch tip-stalling" . however i dont know what to do about it (other than reducing the angle once it approaches critical). Need input please.

Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
tobias, Thu Jun 28 2012, 02:04AM

Does it needs to have this configuration? Why not to go for a proved/simple design?
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Thu Jun 28 2012, 02:53AM

tobias wrote ...

Does it needs to have this configuration? Why not to go for a proved/simple design?
this design was choosen for some of the advantages over the quad rotor, like better lift better flight time, and most importantly a can have better views of the compition arena for my sensors...but the liability is that its more difficult than a quad to stabilize.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Sat Jun 30 2012, 12:34AM

It works ! ! ! * (though I did crash it)

Pitch instability problem... solved!
Roll oscillations... solved!



It can lift more than 1.7Kg's! AUW (3.7 pounds)
landing gear will be changed to the 700 sized heli skids.







Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Carbon_Rod, Sat Jun 30 2012, 01:43AM

You will need to calculate lift over flight-time at operational altitude.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Sat Jun 30 2012, 02:44AM

Yes, that will be the next step, controllibility first, then capability...
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Sun Jul 01 2012, 03:43AM

Video please? What was the final configuration?
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Sun Jul 01 2012, 06:01AM

AndrewM wrote ...

Video please? What was the final configuration?
yep let me post a pic for now, im trying to figure out how to use a GoPro ATM.


1341122499 2431 FT136218 Sam 0005

1341122499 2431 FT136218 Sam 0009
I crashed it after i "whiskey throttled" the collective. But im rebuilding now, fortunately tilt rotor with fixed pitch dont have all the expensive little parts that helis have.


Im hoping this among other sources will help me avoid saturation of the several integrals ill be maintaning... Link2

Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Sun Jul 01 2012, 08:50AM

Good stuff! I see you're not using the wooden pole to damp oscillations any more. How did you get rid of that? From the pics it looks like you're dangling the battery pack underneath now.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Sun Jul 01 2012, 11:40AM

Steve Conner wrote ...

Good stuff! I see you're not using the wooden pole to damp oscillations any more. How did you get rid of that? From the pics it looks like you're dangling the battery pack underneath now.
First, as for the pole. Yes we've done away with it, now that ive pushed some mass out left and right, those rotational moments are slower and the gyro+math can keep up from the kk board.

second, hanging the battery was a huge help, and remember i said i was wondering if the CL should be well above the CG, well it pretty much has to be (a pendulum) or pitch changes are erratic or have no effect.

i like this more than my quad, as theres half the props, half the motors, and half the ESCs, so its cheap to fix. And a camera/sensors are easier to mount with better field of view than from a quad.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Tue Jul 03 2012, 03:13PM

VIDEO!!!

You've just built a tiltrotor, you really expect me to believe you can't figure out how to upload some vids?
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Tue Jul 03 2012, 05:32PM

AndrewM wrote ...

VIDEO!!!

You've just built a tiltrotor, you really expect me to believe you can't figure out how to upload some vids?

i can build UAVs, and plan to build spacecraft, but they still wont give me a degree in EE!
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Tue Jul 03 2012, 09:49PM

You don't need a degree in EE to operate a GoPro! Vids or it didn't happen smile

PS: You might need one before anyone will let you near a spacecraft.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Tue Jul 03 2012, 10:18PM

Steve Conner wrote ...

PS: You might need one before anyone will let you near a spacecraft.

Ha, if that was the requirement nothing would ever get built around here! Based on the number of connector jackposts that get twisted off, inspection mirrors shorting out battery cells, and ESD bags left over TC&R antennas I'd wager a HS diploma isn't even a requirement...


I propose a boycott of all of Patrick's threads until he posts video.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jul 04 2012, 02:21AM

AndrewM wrote ...

I propose a boycott of all of Patrick's threads until he posts video.
ok ok ill post one tomorrow for sure, my fiberglass landing skid is a little weak at the moment though.



As for Steve Connor's point, highly educated idiots F things up all the time... those NASA idiots blew up 2 space shuttles killing 14 with nothing more than their own incompetence.

Id rather have competent people without degrees, than incompetent idoits with degrees. Especially if im the one sitting on 800 tons of ammonium perchlorate.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Thu Jul 05 2012, 11:39PM

OK video on the way!!!

EDIT: im in the middle of a california forest and my cell-interent connection isnt worth a dam atm. sorry.

heres a more primative tilt rotor with 3 motors... Link2

Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Fri Jul 06 2012, 06:05AM

You disappoint me. :(
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Fri Jul 06 2012, 01:46PM

The Panther looks cool, however I'm disappointed that the rear rotor doesn't tilt backwards and act as a third propeller when transitioning to flight. :( Maybe they decided that it wasn't worth the extra complexity, but it would have looked neat.

Did I mention, we want video! >____>;

I also think it is a tad unfair that so-called grown-ups get to spend defence money on building RC planes and playing with them.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Fri Jul 06 2012, 11:06PM

it looks like they turn it off when they dont need it, thats why i said its more primative then mine or any true tilt rotor. they effectivley have a tri rotor some of the time, then dead wieght the rest of the time... every ounce of dead whiegt means an ounce of battery, fuel, bullets or High explosives not carried to the battlefield. cool idea but still primative.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Mon Jul 09 2012, 07:37PM

Video!



fast forward to 3:25 to see it really fly.

eventually i get it to fly, break a prop and most of the other good flying happens off camera. But this isthe best i have.

its too unstable with just 3 gyros, it really needs 3 accelerometers, even my ace test pilot Corey Kohler is pressed to the limit to keep it in a hover.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Mon Jul 09 2012, 10:02PM

Yay video thanks!!

That rod is doing you zero good if its not fastened on tightly. Also from the looks of things you need a rod or something stabilizing the pitch direction too.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Mon Jul 09 2012, 10:06PM

AndrewM wrote ...

Yay video thanks!!

That rod is doing you zero good if its not fastened on tightly. Also from the looks of things you need a rod or something stabilizing the pitch direction too.
yep before i had the GoPro cam, i did have two good sticks on there and the fastend better, it did make a differecne.

really, the sticks help stability, yet there best purpose is saving props.

EDIT 5:10pm : ive solved the roll oscillation again, by readjusting the roll pot with two better sticks attached. Then crashed it in real bad, striped the titanium gears again. dam it.


Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Tue Jul 10 2012, 04:31PM

ok ive been folowing the explanations from these two sites:

Link2 PID in C code for position.

Link2 math and reasoning behind both velocity and position PIDs.

which parts in the below pic are the P the I and the D ?

1341937897 2431 FT136218 Image320
im thinking the first part up to the + sign is the P, then the I and last the D, and is that "K sub 0" or "K sub i"?


Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Ken M., Tue Jul 10 2012, 04:51PM

ATM I can't find it but I know In a previous version of Aeroquad had the arduino code for a PID loop but heres a Link to the repository. Link2
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Tue Jul 10 2012, 05:44PM

That code appears to be differentiating position feedback to get velocity. You, on the other hand, have a gyro so you can get velocity data directly.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Thu Jul 12 2012, 02:34AM

IMPROVED!


1342060646 2431 FT1630 Sam 0013h



its now easy enough for any dope to fly.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
AndrewM, Thu Jul 12 2012, 07:04AM

Wee, looking better.

Are you still limited to hops like that or have you achieved longer flights?
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Thu Jul 12 2012, 07:07AM

i can muddle along in 10-15 second sloppy hovers.
If i change my dual rates and exponential i think i can get it stable for minutes at a time. Ill do this first thing tomarrow.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Sun Jul 15 2012, 02:58AM

ok Ive been doing some thinking...

i want to use a ramp, to initially change acceleration states, this will avoid wind-up errors in domain, while setting a maximum velocity allowable will avoid wind-up in range.


ive also been looking at tinkerforge: Link2




1342343972 2431 FT1630 Imu Math Magic

Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Tue Jul 17 2012, 05:29AM

new vids




1342508958 2431 FT1630 Pi Controller
the first step, a PI loop.
SP = setpoint (input form pitch stick), m/s
PV = process variable (output for feedback), m/s
MV = Manipulated variable (control signal out), degrees of tilt.

so for this PI loop , i would assign meter per second values to pitch stick position (fore and aft speed) then use the accelerometer to judge the current velocity, and adjust as needed. Then repeat as funtion prototype calls for each axis.

but as for the ugly part, the gyros must be able to contribute too !? so how do i let the accelerometers have there say and then the gyros? Obviously, the accels are responsible for translation, the gyros for rotation.

is it possible that i have to run two PIDs in parallel one the the gyro's commanded tilt (position PID), the other for the accelerations needed duration, (the velocity PID?).?


EDIT: if the gyro PI tilts then degees/seconds are output, while the Accel PI keeps track of velcity/time. If that is the case then i think the two must be in series, not parallel as i wrongly stated above..
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
WaveRider, Tue Jul 17 2012, 01:44PM

If you want full sensor fusion between accelerometers , gyros, even visual, GPS and user data, you can't beat the Kalman Filter approach. You are on the right track with the PID controllers. What is missing (as you discovered) is a way to put all the sensor data together. The Kalman filter's ability to handle vectorized data is very convenient..but can get cumbersome particularly if non-linear physical models are used.


Link2
Link2
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Tue Jul 17 2012, 08:24PM

OK, if started a post with DIY Drones, under the screen name "Test Pilot Mafia" unfortunately my post is going unseen, this has happened before in other places too.

Me -> Link2


edit: pendulum-cart model : Link2

bicopter: Link2

Quote: "The SCORPID-500 is now fully stabilised and controlled by a 9 DOF IMU (ArduIMU+ v2, HMC5843, GPS with firmware TriStab v3.3 JLN). The SCORPID-500 VTOL UAV uses an innovative design based on Gary Gress concept from Gress Aero. The Oblique Active Tilting (OAT) at 45° of the twin engines allows a full pitch control by using the induced gyroscopic moment."

OAT = oblique active tilting, Link2





1342595449 2431 FT1630 Vtol



1342593226 2431 FT1630 Oat4
note the angle allows a single tilt axis to cross both the roll and pitch planes!




Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jul 18 2012, 09:33PM

OAT = Oblique Active Tiliting, singular or dual.

the OAT allows landing on tilted surfaces, which quads and tri's cant do.

PDF:
]oat.pdf[/file]

Ive been told/fear that possibly my current design wont work. supposedly (and theres no documentation from kkmulticopter) you would need a low (long vertical destance) CG and a very low inertia prop/motor combo. or the system has no hope of becoming stable.

My design was the typical FAAT type tilt rotor, but the OAT may be far better, especially for smal compact UAVs.



Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Tue Jul 24 2012, 02:32AM


1343100609 2431 FT1630 Sam 0059abc
Its still wont hold a hover but at least i can show definate pitch control.

OK, with the above ive just demonstrated that :

1) yaw works as predicted.
2) using gyro scopic forces does indeed effectively control pitch.
3) the gyro prop idea (Greg Gress) seems to still work with the KKmulticopter/flycam/twin copter board.

So, OAT is defineatly superior to FAAT (fore aft active tilting)...
I plan to switch from the primative KK/flycam baord to the HK 2.0 board seen here. Link2

the problem with the flycam boards is that they seem primative, with no advice or specs given to build the airframe, for 140$ you get the board and some simple instructions and settings, but nothing more. And ive been told that the KK boards dont have PIDs, Kalman filters or any of the usuall stability strategies, if true i dont know how it works, just those three magic potentiometers. it has only gyros.

the HK 2.0 board has an LCd screen, buttons, and an editor to change PI, PD, PID type settings, for each axis for upto eight motors, it has both accelerometers and gyros. All for just $34.


Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Wed Jul 25 2012, 03:50AM

Servos !!!


1343188216 2431 FT136218 Sam 0065large
Tiny, Tiny, Tiny... Beefy, Beefy, Beefy

So far we have:
two Castle ESCs 50 amp upto 34 volts. (w 5 amp BEC)
two e-flite power 10 motors.
10 x 3.8 props ccw and cw. (APC props)
one Flycam Blackboard. (Twin Copter Flash)
two savox micro servos. (SH-263-MG)
two MKS digital, metal gear servos, standard size 140oz torque, (DS1009)
8 plastic servos analog.
one lipo 14.8 4 cell, 2200mah
one lipo 11.1 3 cell, 2200mah
one HiTec X4 charger


1343191479 2431 FT1630 Sam 0068ad




Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Thu Jul 26 2012, 10:31PM

Changes have been made to the wing torque tubes:

1343350192 2431 FT1630 Coupler
Left and right torque tube couplers. as planned to be made.

MWC, se type controller:
] newbies_guide_to_setting_up_crius_multiwii_se_boar d_v4-22-12.pdf[/file]

OK ive made the decision to buy the HK 2.0 controller:


1343341860 2431 FT136218 A
Graphics for configs and prop direction.


1343341860 2431 FT136218 B
real-time IMU checking.


1343341860 2431 FT136218 C
Menus


1343341860 2431 FT136218 D
PID and such settings, no laptop or Basp needed.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Steve Conner, Fri Jul 27 2012, 10:15AM

Nice, how does it compare to the OpenPilot system?
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Fri Jul 27 2012, 07:01PM

Steve Conner wrote ...

Nice, how does it compare to the OpenPilot system?
well the HK and Crius MWC controllers support bicopter mode, but open pilot seems not to.

i think i stick with what other bicopter piltos are using, just so i have people to help me when stuff stops working right.
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Fri Sept 28 2012, 06:27AM

New big devlopements are on the way... Multi wii (Crius AIO type) with variable PIDs on each axis has been assembled, testing to come this weekend... its been awhile since ive posted here, but ive been continuously working on it...
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Fri Sept 28 2012, 09:44PM

Swiss cheese anyone?


1348868656 2431 FT136218 Sam 0319
Re: CSU Chico Tilt Rotor Flying Machine, (Airframe and Electronics, 2 of 3).
Patrick, Thu Oct 04 2012, 05:33AM

Building continues....

Balsa Article:
Link2


1349328793 2431 FT136218 Sam 0326

1349328794 2431 FT136218 Sam 0328

1349328794 2431 FT136218 Sam 0330

1349328794 2431 FT136218 Sam 0338