Marshall Technical Reports Server

Field Programmable Gate Array for Implementation of Redundant Advanced Digital Feedback Control

NASA/TM-2003-212501, King, K.D., Field Programmable Gate Array for Implementation of Redundant Advanced Digital Feedback Control, George C. Marshall Space Flight Center , Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546-0001, June 2003, pp. 20, Format(s): PDF 204k

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The goal of this effort was to develop a digital motor controller using field programmable gate arrays (FPGAs). This is a more rugged approach than a conventional microprocessor digital controller. FPGAs typically have higher radiation (rad) tolerance than both the microprocessor and memory required for a conventional digital controller. Furthermore, FPGAs can typically operate at higher speeds. (While speed is usually not an issue for motor controllers, it can be for other system controllers.) Other than motor power, only a 3.3-V digital power supply was used in the controller; no analog bias supplies were used. Since most of the circuit was implemented in the FPGA, no additional parts were needed other than the power transistors to drive the motor. The benefits that FPGAs provide over conventional designs—lower power and fewer parts—allow for smaller packaging and reduced weight and cost.
Keywords:field programmable gate, array, digital, microprocessor, controller, radiation, motor, static, random, triple-modular redundancy, serial, receiver, interface, generator
Subjects:Engineering: Electronics and Electrical Engineering: Circuitry
Engineering: Electronics and Electrical Engineering: Feedback and Control Theory
Engineering: Electronics and Electrical Engineering: Electronic Components
ID Code:634
Deposited On:15 September 2003