Title :
Distributed Motor Controller (DMC) for operation in extreme environments
Author :
McKinney, Colin M. ; Yager, Jeremy A. ; Mojarradi, Mohammad M. ; Some, Rafi ; Sirota, Allen ; Kopf, Ted ; Stern, Raivo ; Hunter, Don
Author_Institution :
Jet Propulsion Lab., Pasadena, CA, USA
Abstract :
This paper presents an extreme environment capable Distributed Motor Controller (DMC) module suitable for operation with a distributed architecture of future spacecraft systems. This motor controller is designed to be a bus-based electronics module capable of operating a single Brushless DC motor in extreme space environments: temperature (-120°C to +85°C required, -180°C to +100°C stretch goal); radiation (>;20K required, >;100KRad stretch goal); >;360 cycles of operation. Achieving this objective will result in a scalable modular configuration for motor control with enhanced reliability that will greatly lower cost during the design, fabrication and ATLO phases of future missions. Within the heart of the DMC lies a pair of cold-capable Application Specific Integrated Circuits (ASICs) and a Field Programmable Gate Array (FPGA) that enable its miniaturization and operation in extreme environments. The ASICs are fabricated in the IBM 0.5μm Silicon Germanium (SiGe) BiCMOS process and are comprised of Analog circuitry to provide telemetry information, sensor interface, and health and status of DMC. The FPGA contains logic to provide motor control, status monitoring and spacecraft interface. The testing and characterization of these ASICs have yielded excellent functionality in cold temperatures (-135°C). The DMC module has demonstrated successful operation of a motor at temperature.
Keywords :
BiCMOS analogue integrated circuits; application specific integrated circuits; brushless DC motors; distributed control; field programmable gate arrays; machine control; space vehicles; ASIC; ATLO phases; DMC; FPGA; IBM silicon germanium BiCMOS process; analog circuitry; brushless DC motor; bus-based electronics module; cold-capable application specific integrated circuits; distributed motor controller; extreme space environments; field programmable gate array; future spacecraft systems; sensor interface; size 0.5 mum; spacecraft interface; status monitoring; telemetry information; Actuators; DC motors; Field programmable gate arrays; Motor drives; Silicon germanium; Space vehicles; Wiring;
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4577-0556-4
DOI :
10.1109/AERO.2012.6187248