http://dl.dropbox.com/u/2689187/tesina_Hector.pdf Leandro, I'm interested as well in your bachelor thesis :P, I'm looking forward to see what you have done to Mentor xDD Cheers. On Thu, Jun 9, 2011 a
Prof Warmers and Leandro, here it ismy master thesis. It has been written in Spanish, but I think the maths, implementation and results can be followed without problems despiting the language. http
Bruzzlee, you should create a branch containing the things you want merged. Push this branch to your own github repo (your fork), then issue a pull request for integration of this into the dev branch
Hector, it would be nice if you send me your thesis. Tanks Heinrich Hector Garcia de Marina schrieb: Hi Bruzzle, I had the same issues about pressure sensors. I solved it applying an IIR filter (Butt
@ Felix The AoA Module needs changes in the estimator and there is a pitch switch in the pitch loop of stabilization. Maybe it needs a short description for the usage in the airframe. If you create
@ Felix The AoA Module needs changes in the estimator and there is a pitch switch in the pitch loop of stabilization. Maybe it needs a short description for the usage in the airframe. If you create a
U'r welcome I saw there is a new ArduIMU sourcecode. I just want to warn you that my assumption don't have to be consistent with the new code. Question: Anyone have tried the new code for a bungee ta
Hi, i think one of the problem is the fact that in the cross product of a=W x V (rates cross speed over ground) only the yaw rates are taken into account to correct the gravitation vector to fly long
same scenario, but this time, i also made the filter without heuristic use the magnetometer for yaw only ( I believe that is what arduimu does ). You notice that the error is even worse ( up to 35 de
Hi, The arduimu_basic code has some special tricks to try to detect high acceleration when launching (high throttle, low speed) and prevents the imu from using accelerometers. I'm still removing some
Hi We're using the arduino-basic code and the Kalman Filter for GPS-Data Dennis Am 14.05.2011 05:15, schrieb antoine drouin: Hi Dennis What filter are you using ? On Sat, May 14, 2011 at 12:38 AM, La
the arduimu dcm does not compute dV/dt to correct X (yet). It can be added. But probably a limiter on the x- accelerometer measurement would be good too (better?) to clip off anything above 0.8g sinc
Hi all We would like to develop an autonomous Bungee-Takeoff. We have written a routine that actually works. In the first seconds of the start it looks very good. But then the UAV starts to decline a
Hi Chris, congratulations to your awesome flight! Can you put this info (some pictures are also welcome) on the wiki under: http://paparazzi.enac.fr/wiki/Airframes or http://paparazzi.enac.fr/wiki/Ha
Here are some more data that i forgot to mention: AUW was exactly 5Kg but the plane could lift that weight without a problem and glide nicely for a brick. Landing speed (manual landing) was awfully h
Hi, can you tell what's your video transmitter? regards Rui Costa On Sat, Dec 4, 2010 at 8:02 AM, Chris <address@hidden> wrote: I went the other way :-) Having constructed 5 airframes from g
I went the other way :-) Having constructed 5 airframes from gliders to delta wings but finally i understood that long flight time is not the same as long range. After some tests i concluded that foa
Also, before I have another crash, when I edit the waypoints and input an altitude, do I input a desire altitude reference from 0m or do I enter and altitude plus the ground altitude at that spot? I
Yes, I launched in Auto1 as it was described in the manual. I did have very little authority on the aircraft in Auto1 and I could not recover on time. It just nose dove inverted and hit the ground ha