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David L Augenstein, Age 59339 Manhattan Ave, Hermosa Beach, CA 90254

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Known as:
David S Augenstein Dave L Augenstein Davi Augenstein Augenstein Davi Laurence Fuller

David Augenstein Phones & Addresses

339 Manhattan Ave, Hermosa Beach, CA 90254 (310) 376-5405 (310) 379-5895

341 Manhattan Ave, Hermosa Beach, CA 90254 (310) 376-5405

120 Longfellow Ave, Hermosa Beach, CA 90254

Huntington Beach, CA

Glen Arbor, MI

Hawthorne, CA

Los Angeles, CA

Orange, CA

Manhattan Beach, CA

West Lafayette, IN

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David Augenstein resumes & CV records

Resumes

David Augenstein Photo 10

Senior Project Manager

Location:
Hermosa Beach, CA
Industry:
Defense & Space
Work:
Boeing
Satellite System Engineer Boeing
Senior Project Manager
Skills:
Project Management, Program Management, Integration, Process Improvement, Leadership, Engineering, Management, Project Planning
David Augenstein Photo 11

Behavior Interventionist

Location:
Hermosa Beach, CA
Work:
Behavior Frontiers
Behavior Interventionist
Education:
University of California, Los Angeles
Bachelors, Bachelor of Arts

Publications & IP owners

Us Patents

Attitude Determination System And Method With Outer-Loop Gyro Scale-Factor Non-Linearity Calibration

US Patent:
6615117, Sep 2, 2003
Filed:
Nov 13, 2001
Appl. No.:
09/993022
Inventors:
Rongsheng Li - Hacienda Heights CA
David L. Augenstein - Hermosa Beach CA
Assignee:
The Boeing Company - Seattle WA
International Classification:
G06F 1900
US Classification:
701 13, 701221, 701214, 34235714, 244158 R
Abstract:
A method and apparatus for calibrating rate sensor measurements to compensate for rate sensor scale factor non-linearities. An outer loop compensator compares current rate sensor scale factor estimates with the current scale factor non-linearity compensation, and deviations from the current non-linearity compensation are corrected in an updated compensation.

Dual Spin Zero Momentum Satellite System

US Patent:
6152402, Nov 28, 2000
Filed:
Apr 7, 1999
Appl. No.:
9/287721
Inventors:
David L. Augenstein - Hermosa Beach CA
Assignee:
Hughes Electronics Corporation - El Segundo CA
International Classification:
B64G 128
US Classification:
244164
Abstract:
An attitude control system for a spacecraft which includes a bearing power and transfer assembly. The bearing power and transfer assembly is disposed between a first body and a second body. The first body and the second body are counter-rotated with respect to each other by the bearing and power transfer assembly such that the overall spacecraft momentum about the spin axis of the bearing and power transfer assembly is nominally zero.

Method And Apparatus For Controlling Spacecraft Attitude With Rotational Star Trackers

US Patent:
6236939, May 22, 2001
Filed:
Mar 3, 1999
Appl. No.:
9/261727
Inventors:
Douglas H. Hein - Los Angeles CA
Garry Didinsky - Niles IL
David L. Augenstein - Hermosa Beach CA
Assignee:
Hughes Electronics Corporation - El Segundo CA
International Classification:
G01C 2102
G06G 778
US Classification:
701222
Abstract:
High precision spacecraft attitude determination is produced by specially positioning the spacecraft's star trackers and then filtering out measurement errors produced from star tracker electronics. In addition to the conventional azimuth and elevation controls used for star tracker pointing, the star tracker detector array is rotationally positioned about its boresight so that its pixels are traversed by the imaged star path at an angle within 20. degree. of diagonal. This forces both vertical and horizontal spatial error components in the detector plane to a high frequency range at which they can easily be filtered out in common.

Possible Relatives

Daniel W Augenstein  Jennifer J Augenstein  Jeremy H Augenstein  Robert A Augenstein  Stephen Augenstein  William G Augenstein  Amy L Augenstein  David J Last  David K Stancil  David J Stancombe 

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