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Oded D Lerner

from San Jose, CA
Age ~84
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Also known as:
Oded Amy Lerner, Oded C Lerner, Oled Lerner
Phone and address:
1960 Meridian Ave, San Jose, CA 95125
(408) 264-4411
Related to:
Alon Markowitz, 62Joe R Jones, 75John H Jones, 39Jacqueline F Dudley, 35
Connected to:
Aaron Lerner, 49Adina J Lerner, 64Alejandro D Lerner, 57Alyson J Lerner, 54Ana A Lerner, 74Andreas P Lerner, 36Arthur Lerner, 100Brad D Lerner, 66Bruce L Lerner, 70Cara G Lerner, 50

Oded Lerner Phones & Addresses

  • 1960 Meridian Ave, San Jose, CA 95125 (408) 264-4411
  • 1750 Stokes St, San Jose, CA 95126 (408) 288-8406
  • 1800 Stokes St, San Jose, CA 95126 (408) 288-8406
  • Torrance, CA
  • 4402 65Th St, Seattle, WA 98115 (206) 525-8006
  • Los Angeles, CA

Work

Company: Dell computers 2010 Position: Power system engineer

Education

School / High School: TECHNION (ISRAEL)- , 1964 Specialities: BS in ELECTRICAL ENGINEERING

Skills

Power Electronics inovative design Conc...

Industries

Aviation & Aerospace

Resumes

Resumes

Oded Lerner Photo 1

Principal E E

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Location:
San Francisco, CA
Industry:
Aviation & Aerospace
Work:
ROCKWELLCOLLINS since Sep 2002
PRINCIPAL E E
KAISER ELECTRONICS since Jan 2001
Principle Engineer
Rockwell Collins 1990 - 2009
Principal EE
HONEYWELL INTERNATIONAL Jan 1999 - Jan 2001
Principal Staff Engineer
PRIMEX AEROSPACE (General Dynamics) Jan 1997 - Jan 1999
Senior Staff Engineer
Education:
Technion-Machon Technologi Le' Israel 1964 - 1968
BSEE, ELECTRICAL ENGINEERING Technion-Machon Technologi Le' Israel 1963 - 1967
BSC, ELECTRONICS
Skills:
Electronics
Pcb Design
Aero Space Power Systems
Systems Engineering
Sensors
Engineering
Digital Power Electronics
Oded Lerner Photo 2

Oded Lerner

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Work:
DELL COMPUTERS

2010 to 2000
Power System Engineer
GENERAL ELECTRIC
Minden, NV
2010 to 2010
Consulting Engineer
ROCKWELL COLLINS
Silicon Valley, CA
2009 to 2009
Principle Engineer
HONEYWELL INTERNATIONAL
Redmond, WA
1999 to 2002
Principal Staff Engineer, Radar Group
GENERAL DYNAMICS (PRIMEX)
Redmond, WA
1997 to 1999
Senior Staff Engineer, Space Power Electronics Department
Education:
TECHNION (ISRAEL)
,
1964 to 1968
BS in ELECTRICAL ENGINEERING
Technion
,
1964 to 1968
BS in Electronics
ISRAELI INSTITUTE OF TECHNOLOGY
,
BSEE
Skills:
Power Electronics inovative design Concept to hardware delivary Analog/digital Analysis Documentation

Publications

Us Patents

Automatic Gain Control Of A Torque Sensor For A Power Assist Steering System

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US Patent:
57522081, May 12, 1998
Filed:
Sep 29, 1995
Appl. No.:
8/538496
Inventors:
Oded Lerner - Torrance CA
Assignee:
TRW Inc. - Lyndhurst OH
International Classification:
B62D 504
US Classification:
701 41
Abstract:
A control circuit (33) controls the gain of a torque sensor (32) of a type providing two output signals (V. sub. 02, V. sub. 03) where the two output signals have values functionally related to a value of an input drive signal (V. sub. D) and torque sensed by the torque sensor. The two values varies substantially equally and oppositely from each other in response to sensed torque. A variable gain amplifier (36) provides the input drive signal. A rectifiers/filters circuit (38) monitors the two output signals of the torque sensor. A gain control circuit (50) controls the gain of the drive signal in response to the sum of the monitored two output signals of the torque sensor relative to a reference voltage.

Solar Array Maximum Power Tracker With Arcjet Load

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US Patent:
56044305, Feb 18, 1997
Filed:
Oct 11, 1994
Appl. No.:
8/322122
Inventors:
Darwin K. Decker - Hacienda Heights CA
Donald L. Baxter - Redondo Beach CA
Oded Lerner - Torrance CA
Jeffrey D. Campbell - Hawthorne CA
Richard A. Rosenthal - Redondo Beach CA
Michael J. Cook - Garden Grove CA
Assignee:
TRW Inc. - Redondo Beach CA
International Classification:
G05F 1565
G05F 500
H02M 744
H02J 700
US Classification:
323275
Abstract:
A solar array maximum power point tracking system for regulating the power output of a solar array associated with a spacecraft. An on-board computer measures the bus voltage and current from the solar array and generates a power calculation of the solar array power output. The on-board computer applies a first reference signal to a remote error amplifier representative of an incremental change in the solar array power. Additionally, the solar array bus voltage is applied to the remote error amplifier such that the remote error amplifier senses the solar array bus voltage and generates an output voltage indicative of the change of the solar array power. The output voltage of the error amplifier is applied to a power processor unit. The output voltage from the remote error amplifier and the bus voltage are applied to a power stage within the power processor unit. The power stage generates an output current that is applied to an arcjet thruster.
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Oded D Lerner from San Jose, CA, age ~84 Get Report