Other Parts Discussed in Thread: LMP2012, LMP2012QML, LMP2021, LMP2011
Hello,
We are developing payloads for space missions (Mars rovers for 2020) and we have some important doubts regarding part LMP2012/LMP2012QML
which we need to be resolved to ensure the functionality of our designs.
We see that the typical values of bias current are -3pA (same for space model and commercial model), there is also a graph in the commercial model datasheet which implies that Ibias could be around around 100 pA depending on Vcm.
Nevertheless, we have done some designs to measure this current (Transimpedance configuration with resistor and integrator configuration with capacitor to measure the slope of the bias current ramp) and it appears to be much higger (400-800pA), we have also found an open question (which haven’t been answer yet) regarding this issue here:
https://e2e.ti.com/support/amplifiers/precision_amplifiers/f/14/p/541206/1985485#1985485
We are aware that trying to measure this magnitude of bias current is a delicate issue and that maybe our test boards for this are not well optimized, however we need to be sure that the values that we sense are wrong and that the real ones are those provided by the datasheet so it is safe to ask you about it. It would be great to have some clues in how you measure this currents in order to replicate it in our lab.
So to sum up, questions are:
1) Are the datasheet values of Ibias correct?
2) What are the Max/Min values for this parameter? We haven't seen it in the datasheets.
3) If it is possible, how can we replicate the measurements of this values in our lab?
Thank you very much in advance!