ricci2
Second Officer
Flight distance : 61158 ft
France
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Beard Posted at 2017-4-3 10:42
Nil, great method. I've been thinking about this over the weekend...scary..as I am unqualified to do so. What is the point of inputting the Z COG since that will change after the landing gear retracts? After adding a custom gimbal to ours we left the Z at -230 and noticed no irregularities. Alternatively, if one is more concerned with positioning wouldn't one be more concerned with the measurement from the base of the GNSS antennae/receiver....and considering that the M600 does not carry a survey grade receiver then the error of the Z will be more than the the total height of the airframe anyhow? Any insight is appreciated.
Hi Beard,
Theoretical maths and real world maths often part company when extraneous factors influence the result unless all the varying anomalies are all taken into consideration as we know by trying to predict the weather. Kover, initially asked for the theoretical COG for some bureaucratic paperwork so he could fly in his country, why knowing the Cog of a craft that has a mass of 9.6kg has to do with things is beyond me, its probably the paper work for a full sized aircraft schedules. sorry off topic, you make a good point which is why I calculated using the supplied CAD drawing but alas it was only for the M600 but as a paperwork exercise it would be enough to give Kover the number to tick a box on the forms and it was a DJI supplied drawing.
The Cog of a dynamic object not on a fixed orbit and influenced by exterior vector forces like wind, pitch and yaw, will have very little chance of being calculated to any accuracy, however; with DJI’s altitude control mechanisms, stability is very good so maybe when the craft is geostationary it might have an almost static Cog, then Gravity gets involved so altitude is a factor, the plight continues infinitum.
Nil was pointing out a practical way to find a static Z, coordinate to meet Kovers needs I believe and it will not relate to the X,Y,Z, coordinates for the IMU, because if they did every craft will be different due to the payloads. The Imu and flight controllers as far as I can calculate needs the centre of inertia for the craft as do the gps antennas, accelerometers because they all need a point in space to reference themselves too so they can calculate how much correction to apply to maintain an equilibrium around that point which is why the 230mm works. It puts the Centre of inertia around 26mm below the top plate of the M600 and the Cog 54mm below the bottom plate (No camera or gimbal).
Lastly I have experimented by moving the IMU and gps X and Y, position to see what effect it had apposed to the Z, position. Results: the Z, axis had no visual effect when moved 100mm down, the X and Y, showed visual signs of drifting when altered 100mm out. You can draw your own conclusions; however keep in mind this was a visual conclusion.
Sorry if I have confused matters.
ricci
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