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B. Blaes
Also published under:B. R. Blaes
Affiliation
Jet Propulsion Laboratory, Pasadena, CA, USA
Topic
Angular Speed,Baseband Signal,Closed-loop System,Dcdc Converter,Digital Circuits,Digital Signal Processing,State Machine,Amount Of Rotation,Analog-to-digital Converter,Automatic Gain Control,Bias Voltage,Block Diagram,Bytes Of Data,Changes In Gain,Circuit Design,Closed-loop Control,Closed-loop Control System,Closed-loop Frequency Response,Collaborative Efforts,Continuous Operation,Control Filters,Control Loop,Control Synthesis,Control System,Coriolis Force,Correct Form,Damping Matrix,Diagonally Dominant,Differences In Frequency,Digital Technologies,Disturbance Rejection,Dynamic Test,Electrode,External Capacitor,Finite Impulse Response Filter,Frequency Response,Fundamental Frequency,Future Date,Future Modifications,Gain Region,Ground Plane,Gyroscope,Individual Subsystems,Inertial Measurement Unit,Inherent Asymmetry,Input Amplitude,Integrated Circuit,Jet Propulsion Laboratory,Linear Equation,Linear Filter,
Biography
Brent Blaes received the B.S.E.E (77) and M.S.E.E. (79) from California State Polytechnic Univ. Pomona and is presently a senior member of the engineering staff at NASA's Jet Propulsion Laboratory where he has 26 years experience in analog and digital circuit design, integrated circuit development, and flight electronics. He has worked extensively in the development of test circuits, sensors and measurement techniques for characterizing total dose and SEU effects of CMOS circuits and in the development of magnetic mass-memory devices. He was the chief designer of the Radiation and Reliability Assurance Experiment (RRELAX) which flew on the Clementine-I spacecraft and the cognizant engineer and designer of the Free Flying Magnetometer (FFM) data system. He was the task manager for the New Millennium Programs DS2 Mars penetrator probe Follow-On-Experiment. He is currently leading the development of electronics for the external metrology system on NASA's Space Interferometry Mission (SIM).