Digital fluxgate magnetometer: design notes
IntroductionA modern trend in space research is to use small satellites and rocket payloads as a cost-effective space solution for small commercial companies and university researchers. To be in line with this, developing small, lightweight, but sufficiently sensitive instruments is among the main challenges. Fluxgate magnetometers (FGMs) [1] are 'must-have' instruments on board practically every scientific or commercial spacecraft being used for both research and service purposes. To compare FGMs with other types of magnetometers, it is evident to state that FGMs have no real competitors if precise measurements of the vector magnetic field are necessary [2].An essential technology for electronic unit miniaturisation is the broad implementation of digital data processing that promises almost unlimited resources for reducing mass, dimensions, costs and power consumption, as well as improving usability and flexibility [3][4][5]. Using digital technology is even more crucial because of the usual lack of data transmission channel throughput for small satellites with limited ground support. At the same time the digital implementation of an actual analogue device creates problems related to the discretisation of internal data processing [6,7].A joint team of KTH and LCISR previously developed such a digital FGM-the Small Magnetometer In Low mass Experiment (SMILE) [8]. This paper briefly describes the original design, and focuses on solving the specific problems and trade-offs between the sensitivity, response and stability. A description of the current instrument design is given, followed by a discussion of the analogue and digital circuit noise contribution. Further, a mathematical model of the whole magnetometer is presented, with a detailed discussion of the effects of the digital part on the stability and noise levels. The paper also presents experimental data from a recent flight of the instrument on board the ESA REXUS-10 sounding rocket with the SQUID (Spinning QUad Ionospheric Deployer) student payload launched from Esrange in 2011 [9].
Magnetometer designThe magnetometer electronics combines flux-gate sensor analogue front-end circuits with a main digital integrated circuit-a Field Programmable Gate Array (A3P250 FPGA from Actel). The digital correlation algorithm implemented in the FPGA provides the full processing of amplified and digitised fluxgate sensor signals, output data and the necessary dynamics of the analogue feedback voltage. The digital part of the feedback loop programmed in the FPGA allows the generation of a set of parameters necessary for the implementation of a specific application to the given experiment without changing the hardware, which is important for a low budget and time-constrained design.A block diagram of the magnetometer is shown in figure 1, where the main parts are:
AbstractWe presented an approach to understanding the performance of a fully digital fluxgate magnetometer. All elements of the design are important for the performanc...