The data acquisition system COMET developed by Saab AB contains a unit for signal conditioning and A/D conversion, called KSM. The varieties in signal conditioning constitutes of a number of specific PBAs and maintenance as well as reconfiguration of these are complicated not to mention costly. This thesis has aimed to investigating whether the signal conditioning circuits can be replaced by a general purpose, programmable solution. If so, how can this be done? The development has been carried out by evaluating ideas through the use of a laboratory environment and has resulted in an analog design for laboratory purpose. A reconfigurable design is the result of this thesis as an alternative to the solution used today. In the proposed design mainly digital otentiometers, switches and MUXes are used. In that way signal path and overall behaviour can be selected. Some extensions have been made in comparison to the current functionality, but additional development is necessary to make the design complete. Future versions of the COMET system could be significantly improved by considering the result of this thesis when developing the signal conditioning circuitry.

<p>The data acquisition system COMET developed by Saab AB contains a unit for signal conditioning and A/D conversion, called KSM. The varieties in signal conditioning constitutes of a number of specific PBAs and maintenance as well as reconfiguration of these are complicated not to mention costly. This thesis has aimed to investigating whether the signal conditioning circuits can be replaced by a general purpose, programmable solution. If so, how can this be done? </p><p>The development has been carried out by evaluating ideas through the use of a laboratory environment and has resulted in an analog design for laboratory purpose. A reconfigurable design is the result of this thesis as an alternative to the solution used today. In the proposed design mainly digital otentiometers, switches and MUXes are used. In that way signal path and overall behaviour can be selected. Some extensions have been made in comparison to the current functionality, but additional development is necessary to make the design complete. </p><p>Future versions of the COMET system could be significantly improved by considering the result of this thesis when developing the signal conditioning circuitry.</p>

<p>During test flights SAAB uses the data acquisition system COMET 16. The part of the system that receives the signals from the sensors and converts them is called KSM 15. The purpose of this thesis is to develop a data acquisition module on stacked PC/104 modules with a lower production cost. </p><p>Our work has been divided into one part about analog signal conditioning and a second part with digital filtering and memory management of the sampled data. The analog part, designed of regular components like instrument amplifiers, voltage references, operational amplifiers and multiplexers, adjusts the sensors signal levels for the ADC’s that converts the signals. In the digital part the sampling frequency is decimated by digital FIR filters in several stages down to 16 Hz. All the resulting data is temporarily stored in a SDRAM memory before being recovered by the HL-11 board that handles the communication with the other parts of the COMET system. </p><p>We have made a design proposal that needs some additional work and testing before a prototype can be made. It’s primarily the C code in the digital part that needs further development. </p><p>Our result and conclusions should be a great help in the future when developing a small,cheap data acquisition system.</p>

During test flights SAAB uses the data acquisition system COMET 16. The part of the system that receives the signals from the sensors and converts them is called KSM 15. The purpose of this thesis is to develop a data acquisition module on stacked PC/104 modules with a lower production cost. Our work has been divided into one part about analog signal conditioning and a second part with digital filtering and memory management of the sampled data. The analog part, designed of regular components like instrument amplifiers, voltage references, operational amplifiers and multiplexers, adjusts the sensors signal levels for the ADC’s that converts the signals. In the digital part the sampling frequency is decimated by digital FIR filters in several stages down to 16 Hz. All the resulting data is temporarily stored in a SDRAM memory before being recovered by the HL-11 board that handles the communication with the other parts of the COMET system. We have made a design proposal that needs some additional work and testing before a prototype can be made. It’s primarily the C code in the digital part that needs further development. Our result and conclusions should be a great help in the future when developing a small,cheap data acquisition system.