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If you want a closed source turnkey inertial navigation solution, you could look at vectornav.
Otherwise, you should probably go for something similar to the sensors on Pixhawk, but mount them on vibration isolation with a peltier TEC and heatsink providing the weight to make the isolation effective. Control the TEC to keep the board at a constant temperature (25C). This will remove variability of sensor error with temperature so that you can conveniently ignore it.
I have no idea what these cost, but cloudcap sells an IMU and an fully integrated standalone INS+GPS:
http://www.cloudcaptech.com/crista.shtm
The specs in the data sheets are interesting; they go into some detail on how they are quoting rate biases, variances, and such.
My guess is that they are <1k since the nano autopilot is around $1.2k.
Brandon
Always a good question as the term INS gets used different ways. AHRS stands for attitude and heading reference system, as you probably know, so that means a filter which gives you 3D attitude. INS stands for inertial navigation system. Some people use that for a filter which just gives position and velocity, but I was using it to mean a filter which gives attitude/velocity/position.The reason you need GPS (or some other sensor) for an AHRS filter is that you need two reference vector measurements to correct for gyro drift. Those vectors are (typically) the earth's gravity and magnetic field vectors. Magnetometers measure the magnetic field vector, but accelerometers do not measure the gravity vector. Rather they measure the specific force on a proof mass. The specific force is due to gravity and translational acceleration. For a quality attitude estimate you have to estimate the translational acceleration (using something other than the accelerometer measurement itself) so that you can remove that component from the accelerometer measurement. Most methods of doing this use GPS, although people have done it with other things like airspeed. I have a paper pending for the AIAA Journal of Guidance, Dynamics and Control which goes into the subject of the best way to do this for drones flying in turbulence.
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Does anyone know what IMU the DJI A2 uses? Is it thermoelectrically stabilized?
I'm sure that has the same sensors in it as pixhawk, and who knows what "temperature compensated" means for them.
That thing is just kind of a wildcard. You're probably buying the same sensors that pixhawk has and a closed-source software package that is likely to be orphaned.
If you want a constant temp Pixhawk, you could experiment with adding a TEC on a brushed ESC and controlling it with a PID to keep a constant temperature on the mpu6k