I finally did the test of hard fixing the APM case to the frame, thus not having two separate masses with vibration dampening materials in between, as before (i.e. : frame/props on one side and APM on the other side).
This is explain by Forrest Frantz in a post I made earlier about moongel use here:
and in more details here:
I have to say that I felt on my bottom when I saw the results : TWICE less vibrations with this method WITHOUT any moongel nor any other vibration dampening techniques. JUST ONE SINGLE mass (APM fixed on frame directly).
Look at this graph that shows ZACC within plus or minus 0,1g which is twice less than the best +-0,2g I had with moongel combined with rubber bobbins and/or silicon gel. It is measured on the exact same aircraft (except moongel was removed and rubber bobbins were replaced by hard pylons). APM is stcked to the plate with NON foam double sided tape (hard double sided tape, as I did not want to drill screw holes in the APM plastic case).
Not only have I less vibration but I will also get better control on the craft since I get rid of the lag effect of dampening materials.
I confirm thus the theory of Forrest Frantz. It works for my frame.
It would be nice if others could confirm this also on their frame.
I publish this UPDATE after the information about 200hz dangerous vibrations came out thanks to the debate initiated of this post: the APM and its integrated sensor's hardware have a limit (due to low processing power limiting sampling frequency - that should be solved with the more powerful PX4 hardware) in such a manner that all frequencies of 200hz (and multiple of) will impact the APM control (accel) and will go through the 20hz software filter, undetected (thus noise id processed instead of valid signal, possibly creating catastrophies). As there is no way to analyze in a log AccelZ graph if you get these 200 Hz frequencies on your arducopter, it is necessary as a precaution to use dampening technique(s) to eliminate these high frequencies (even if the AccelZ log seems to show low vibrations by direct fixing APM on the frame).
hale Mary ... that thing is beautiful! Never seen such clean work.
It's getting late. my brain died (nothing new). so will look at it tomorrow. thanks for sharing.
Thanks for the kind words, I do custom computer installations for a living and its all about making the wires pretty. I learned from my helicopter days that you need to keep your wires off the sharp edges of the carbon fiber and the neater you keep things the less mishaps you have. It's easy to see things out of place when things are neat. I have some more work to do on the ESC's but wanted to make sure it flew first LOL. I have not tested Loiter yet and unfortunately we are having what is called Santa Anna winds this week end so I think I am grounded. 30 Mph sustained with gusts to 60 Mph.
must have been really tired last night ... didn't notice that these are .rlog
do you have .log files from the flight? you should see a date followed by .log
If you were the boss and sat down to create a project to communicate to your workers, what would be the:
o problem statement
o success criteria
Here you go. I understand what the TLog is which is the telemetry log file. Could you please educate me what the difference between Log and Rlog is?
Beautiful Tri ... great vibration and stability numbers. Thanks for sharing Greg!
From here, you can tune pitch and roll (turn off link the two) and see if you get improvement in stability. But watch for a trade. The X2 was tuned like a cello, but being nearly 2 meters long, you could see the tiny vibrations, so relaxed it a bit. This is your first flight. The best hover is under the horizontal bar on the vibration chart and shows where the statistics are derived. Also, the macro doesn't print the graph in the correct order (biggest numbers first, in your case, z then y, then x) so to see them you sometimes have to right click on the graph and choose data source then click on the z and use the arrows on to the right to move it to the first spot, etc.
Also, your signal to noise proxy is 3. That's good too.
Also note the orange area that tells you your THR_MID. Set that to 593 in MP and next time it will hover at about 50% throttle.
Can you try launching the macro again, now that you know you go after the .log and let me know if the macros fails? Please report the error message if it does. Getting this to work in an international community will be interesting.
"you can tune pitch and roll (turn off link the two)"
I am not sure I understand what you mean here. Are you referring to the Lock Pitch and roll values check box as seen in this screen shot of my config? I had my mid throttle set at 600 and changed it down to 593 per your suggestion. Both those logged flights were not done in real calm winds as I would have liked so the stable hover was not as good as I would like. Those two flights were numbers 2 and 3 on the new copter also my number 2 and 3 on a multicopter so this is all new to me. Thanks for the help. I am glad my patience during the build is paying off in smooth flying so far. I will try the excel sheet again and let you know what happens.
yes, the checkbox.
careful though using it. every time you go back into that page, it is checked even though you unchecked it before. it caused a crash on the X2. my PIDs are unlocked for two reasons: aspect ratio of the prop layout is twice the width (y) than length & uneven distribution of mass in x/y with mass further away from CG in y. in any case, my y P ends up being about twice the x P (and off the chart huge). While tuning live, i made a change to the y P and (not paying attention) it immediately changed the x pid making it about twice what it should be, which as you can imagine immediately sent it into an uncontrolled and wild crash. your PIDs might end up the same, but it's good to check. Generally only the P of the PIDs might be different.
I tried the excel sheet again and did make some progress. First I found in your file config data tab the logdirectory path. I have installed mission planer in a different folder than default so I copied the log files to match the path your sheet is expecting. When I viewed the macros and clicked on main and hit run it asked me to select my log file so good start. Then it gave me this error message. I have Raw logging enabled and you were able to run my two logs so not sure why it sees no data. Do I need to be on a specific tab when I run the macro? There seems to be some sample data in the sheet is this ok?
The advice I give people is to first try removing all isolation methods. Use that result as your baseline. Double sided foam tape is basically a direct mount when it covers the entire back area of the APM. The difference between that and double sided tape (no foam) would be nil. In fact, the foam might actually hold the APM tighter because more of the adhesive will find its way to a surface. The foam is too dense and APM too light to have any measurable isolation impact.
If you keep score on those on this site that have actually made the measurements of before and after, the score is now 7 to 0 in favor of removing isolation systems between the motor and APM. The focus should be on:
o stiffening the frame (tighten bolts, add gussets, use continuous motor masts, etc.)
o balancing the props in axial
o balancing the props in radial
I'm sure there is a case out there where this isn't true, we just haven't seen the before and after proof yet on this thread.
Wish you had the before and after logs so we could see the impact of moon gel on vibration and stability. Glad you didn't crash the ship trying though.
P.S. Isolation is heavily winning (100%) when it comes to isolating the camera gimbal.
Forest since I still am not able to load my log file into your excel sheet I am going to provide you another log with a flight I did today. Please take a look at my vibration graphs. Today I tested the Loiter again and the RTL for the first time. Loiter was rock solid!! I couldn't be happier with how stable and solid it sat in one place. Alt hold worked pretty well but I believe the baro was being affected by the bright sun on the right side of my copter. As soon as I turned it to the left 90 deg it would drop a few feet. I did a test of the baro last night with my flash light and that right side was the side the flash light would change the alt by as much as 2 meters. Today I blacked out the inside of my APM case so I expect that to be more stable now. Going on to my RTL test when I switched into that mode it climbed to the alt it was supposed to and moved back to the home position at altitude really nice. When it reached home position but before it started descending the copter started bucking in place, more so on the second test. I let it be and it started the decent and settled down a lot on the way to 2m and it hovered rock solid there. Can you help me figure out what the bucking is all about at the top of the home way-point before decent?
You are using the version for the old MP logs. I try to delete all of the old versions from the site but apparently missed one. It went after RAW records instead of the new IMU records. It also didn't have the stability analysis.
So try this one. I'll try to find and delete the other.