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Mark Youhanaie

from Westlake Village, CA
Age ~65
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Also known as:
Mark E
Phone and address:
5502 S Rim St, Thousand Oaks, CA 91362
(310) 227-7143
Related to:
Davin Youhanaie, 61Teresa Z Youhanaie, 60Robert E ZintgraffRosa J YouhanaieRebecca L Southwood, 57Richard E Zintgraff, 55Patricia S Zintgraff, 82Cleo ZintgraffBenjamin Youhanaie, 97Robert Edward Zintgraff, 85
Connected to:
Claudia A Youhan, 68Sargon B Youhanian, 77Hanna K Youhanna, 87Tom Youhanna, 52Richard A Youhill, 58Kimberly F Youhouse, 38William F Youhouse, 61Nicole J Youil, 37Hyun Youk, 42Narin Youk, 40

Mark Youhanaie Phones & Addresses

  • 5502 S Rim St, Westlake Vlg, CA 91362 (310) 227-7143
  • Westlake Village, CA
  • 7571 Coastal View Dr, Los Angeles, CA 90045 (310) 670-0534
  • Westchester, CA
  • 3412 Ocean Front Walk, Marina del Rey, CA 90292
  • Playa del Rey, CA
  • Oak Park, CA
  • West Hills, CA

Work

Company: Raytheon 1984 Position: Director

Education

Degree: PhD School / High School: University of Illinois at Urbana-Champaign 1978 to 1984 Specialities: Controls Engineering

Skills

Systems Engineering • Software • Embedded Software

Languages

English

Industries

Aviation & Aerospace

Resumes

Resumes

Mark Youhanaie Photo 1

Consultant

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Location:
5502 south Rim St, Westlake Village, CA 91362
Industry:
Aviation & Aerospace
Work:
Raytheon since 1984
Director
Education:
University of Illinois at Urbana-Champaign 1978 - 1984
PhD, Controls Engineering
Skills:
Systems Engineering
Software
Embedded Software
Languages:
English

Publications

Us Patents

Flir Boresight Alignment

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US Patent:
56728727, Sep 30, 1997
Filed:
Mar 19, 1996
Appl. No.:
8/618646
Inventors:
David F. Hartman - Chatworth CA
Mark Youhanaie - Playa Del Rey CA
Assignee:
Hughes Electronics - Los Angeles CA
International Classification:
F41G 154
US Classification:
250330
Abstract:
A FLIR boresight alignment system (52) for aligning a sensor pod LOS associated with a weapons pod of a fighter aircraft to a navigation reference frame. A pod inertial navigation and global positioning system (62) provides position, velocity and attitude of a sensor (58) within the pod. An aircraft inertial navigation and/or global positioning system (68) provides position, velocity and attitude of the aircraft. The sensor position and velocity and the aircraft position and velocity are applied to a transfer alignment filter (64) that utilizes Kalman filtering. An output of the transfer alignment filter (64) is applied to a sensor inertial navigation system to correct the pod LOS relative to the navigation reference frame. Alternately, the transfer alignment filter (64) may operate directly upon the pseudo ranges and delta pseudo ranges to satellites being tracked by the GPS receiver.

Relative Guidance Using The Global Positioning System

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US Patent:
53441052, Sep 6, 1994
Filed:
Sep 21, 1992
Appl. No.:
7/947623
Inventors:
Mark Youhanaie - West Hills CA
Assignee:
Hughes Aircraft Company - Los Angeles CA
International Classification:
F41G 728
US Classification:
244 314
Abstract:
A method for guiding a vehicle (30) to a target (28) includes furnishing a first vehicle (20) having a first global positioning system (GPS) receiver (24) fixed to receive global positioning signals from a selected constellation (46) of satellites in orbit above the earth and the second vehicle (30) having a second GPS receiver (32) fixed to receive global positioning signals from the same selected constellation (46) of GPS satellites. The first vehicle (20) locates the target (28) with an onboard sensor (26) and converts the location of the target (28) to the frame of reference of the selected constellation (46) of satellites of the GPS. The first vehicle (20) communicates this target position and the available set of GPS satellites to a navigation system of the second vehicle (30). The second vehicle (30) proceeds to the target location provided from the first vehicle (20 ) in the frame of reference of the GPS under control of its navigation system using the positioning signal derived from the second GPS receiver (32) fixed to receive positioning signals from the selected constellation (46) of satellites. In these operations, the second vehicle (30) remains within a sufficiently small operating distance of the position of the first vehicle (20) that variations in systematic bias errors between the first GPS receiver (24) and the second GPS receiver (32) are negligible.
Control profile
Mark Youhanaie from Westlake Village, CA, age ~65 Get Report