Search

Thomas W Holmes

from Napa, CA
Age ~74
Get Report
Also known as:
Thomas Margaret Holmes, Thomas D Holmes, Tom W Holmes, Thomas W Dotson, Thomas Holmen
Phone and address:
2295 Sherry Dr, Fairfield, CA 94558
(707) 257-6705
Related to:
Icholas Holmes, 46Levern HolmesJames W Taylor, 75Margaret A Holmes, 74Linda R Holmes, 72Pi Y Holmes, 79Nicholas D Holmes, 46Authree Taylor, 73Linda C Taylor, 62
Connected to:
Adriene L Holmes, 38Aiessa L Holmes, 45Alamanda S Holmes, 29Aleatrice J Holmes, 80Aleena Holmes, 29Alicia M Holmes, 56Alissa Holmes, 41Allysun L Holmes, 39Andraya Holmes, 34April Holmes, 44

Thomas Holmes Phones & Addresses

  • 2295 Sherry Dr, Napa, CA 94558 (707) 257-6705
  • 511 Elmhurst St, Hayward, CA 94544 (510) 816-0703 (510) 785-1186
  • 1021 76Th Ave, Oakland, CA 94621
  • Vallejo, CA
  • Alameda, CA

Professional Records

Medicine Doctors

Thomas Holmes Photo 1

Thomas M. Holmes

View page
Specialties:
Neurology
Work:
WellStar Medical GroupMarietta Neurology & Headache Center
780 Canton Rd NE STE 400, Marietta, GA 30060
(770) 422-3602 (phone), (770) 421-6115 (fax)
Education:
Medical School
Duke University School of Medicine
Graduated: 2001
Procedures:
Cardiac Stress Test
Hearing Evaluation
Lumbar Puncture
Neurological Testing
Sleep and EEG Testing
Conditions:
Alzheimer's Disease
Anxiety Dissociative and Somatoform Disorders
Bell's Palsy
Carpel Tunnel Syndrome
Dementia
Languages:
English
Russian
Description:
Dr. Holmes graduated from the Duke University School of Medicine in 2001. He works in Marietta, GA and specializes in Neurology. Dr. Holmes is affiliated with Wellstar Kennestone Regional Medical Center.
Thomas Holmes Photo 2

Thomas G. Holmes

View page
Specialties:
Internal Medicine
Work:
Advocate Medical Group
1775 Ballard Rd, Park Ridge, IL 60068
(847) 318-2500 (phone), (847) 318-2966 (fax)
Education:
Medical School
Northwestern University Feinberg School of Medicine
Graduated: 1981
Procedures:
Cardiac Stress Test
Wound Care
Allergen Immunotherapy
Arthrocentesis
Destruction of Benign/Premalignant Skin Lesions
Electrocardiogram (EKG or ECG)
Skin Tags Removal
Vaccine Administration
Conditions:
Abnormal Vaginal Bleeding
Acne
Acute Conjunctivitis
Acute Renal Failure
Acute Sinusitis
Languages:
English
Description:
Dr. Holmes graduated from the Northwestern University Feinberg School of Medicine in 1981. He works in Park Ridge, IL and specializes in Internal Medicine. Dr. Holmes is affiliated with Advocate Lutheran General Hospital.
Thomas Holmes Photo 3

Thomas J. Holmes

View page
Specialties:
Emergency Medicine
Work:
Middlesex Hospital Emergency
28 Cres St, Middletown, CT 06457
(860) 358-8000 (phone), (860) 358-8010 (fax)
Education:
Medical School
Stony Brook University School of Medicine
Graduated: 1991
Languages:
English
Spanish
Description:
Dr. Holmes graduated from the Stony Brook University School of Medicine in 1991. He works in Middletown, CT and specializes in Emergency Medicine. Dr. Holmes is affiliated with Middlesex Hospital.

Real Estate Brokers

Thomas Holmes Photo 4

Thomas Holmes, Florida Agent

View page
Specialties:
Residential sales
Luxury homes
Work:
Champagne & Parisi Real Estate
(561) 706-3203 (Phone)
License #30673245
Client type:
Home Buyers
Home Sellers
Property type:
Single Family Home
Condo/Townhome
Languages:
English

Lawyers & Attorneys

Thomas Holmes Photo 5

Thomas Holmes - Lawyer

View page
Office:
Thomas J. Homes, Esq.
ISLN:
906402557
Admitted:
1975
University:
Boston College, B.A., 1972
Law School:
Suffolk University, J.D., 1975
Thomas Holmes Photo 6

Thomas Holmes - Lawyer

View page
ISLN:
910610542
Admitted:
1993
University:
Rutgers Newark
Thomas Holmes Photo 7

Thomas Holmes - Lawyer

View page
Specialties:
Labor & Employment
School Law
Education & School Law
ISLN:
916637536
Admitted:
2001
University:
Miami University, B.A., 1998
Law School:
Case Western Reserve University, J.D., 2001

License Records

Thomas Ward Holmes

License #:
2263 - Expired
Issued Date:
Oct 16, 1954
Renew Date:
Nov 19, 1985
Expiration Date:
Nov 19, 1985
Type:
Professional Engineer

Thomas E Holmes

License #:
11861 - Expired
Category:
Emergency Medical Care
Issued Date:
Dec 31, 1996
Effective Date:
Feb 4, 2006
Expiration Date:
Dec 31, 2005
Type:
EMT

Thomas Robert Holmes

License #:
MT003185T - Expired
Category:
Medicine
Type:
Graduate Medical Trainee

Business Records

Name / Title
Company / Classification
Phones & Addresses
Mr. Thomas Holmes Jr.
Owner
Cackalak Clothing Co.
Internet Shopping Services
PO BOX, 12061, Columbia, SC 29211
(888) 522-0781
Thomas E Holmes
Thomas E Holmes
Real Estate Agents and Managers
2723 Preston Dr, Mountain View, CA 94040
Thomas Holmes
Vice-President
Container Management Services LLC
Mfg Metal Barrels/Pails
21301 Cloud Way, Hayward, CA 94545
(510) 271-6200
Thomas Holmes
Principal
Tom Holmes
Nonclassifiable Establishments
167 S San Antonio Rd, Los Altos, CA 94022
Thomas Holmes
Manager
HC3 Investments LLC
Thomas Holmes
Chief Executive Officer
Parktoria Technologies LLC
Custom Computer Programing · Custom Computer Programming Services, Nsk
201 Msn St, San Francisco, CA 94105
Thomas R Holmes
HOLMES DEVELOPMENT, LTD
Thomas L. Holmes
OROMEX, INC
Thomas E Holmes
Thomas E Holmes
Real Estate Agents and Managers
2723 Preston Dr, Mountain View, CA 94040

Publications

Amazon

Jeff Daniel Marion: Poet on the Holston

View page

The author of nine volumes of poetry and numerous other writings, the editor of several literary journals, the recipient of copious awards, including the James Still Award from the Fellowship of Southern Writers, and a longtime teacher and mentor, East Tennessee native Jeff Daniel Marion has come to...
Binding

Paperback

Pages

255

Publisher

Univ Tennessee Press

ISBN #

1621901998

EAN Code

9781621901990

ISBN #

15

The Balm of Gilead; or, The Recovery of Man's Fall by Redemption

View page

The balm of Gilead; or, The recovery of man's fall by redemptionThis book published in 1847 has been reformatted for the Kindle and may contain an occasional defect from the original publication or from the reformatting.
Author

Thomas H. Holmes

Binding

Kindle Edition

Pages

31

Publisher

Longman & Co.

ISBN #

9

The Balm Of Gilead: Or The Recovery Of Man's Fall By Redemption (1847)

View page

This scarce antiquarian book is a facsimile reprint of the original. Due to its age, it may contain imperfections such as marks, notations, marginalia and flawed pages. Because we believe this work is culturally important, we have made it available as part of our commitment for protecting, preservin...
Author

Thomas H. Holmes

Binding

Paperback

Pages

68

Publisher

Kessinger Publishing, LLC

ISBN #

1166927563

EAN Code

9781166927561

ISBN #

14

London's Underworld

View page

This book was converted from its physical edition to the digital format by a community of volunteers. You may find it for free on the web. Purchase of the Kindle edition includes wireless delivery.
Author

Thomas Holmes

Binding

Kindle Edition

Pages

174

ISBN #

8

Wikipedia References

Thomas Holmes Photo 8

Thomas Holmes (Executive)

Thomas Holmes Photo 9

Thomas Holmes (Politician)

Isbn (Books And Publications)

Cotton Mather and His Writings on Witchcraft

View page
Author

Thomas J. Holmes

ISBN #

0766166686

Known to the Police

View page
Author

Thomas Holmes

ISBN #

0824062221

Oaklawn Manor

View page
Author

Thomas Holmes

ISBN #

0882894188

Caesar's Conquest of Gaul

View page
Author

Thomas R. Holmes

ISBN #

0404033172

Life Change Events Research, 1966-1978: An Annotated Bibliography of the Periodical Literature

View page
Author

Thomas H. Holmes

ISBN #

0030702879

Life Change, Life Events, and Illness: Selected Papers

View page
Author

Thomas H. Holmes

ISBN #

0275924807

Almost All Are Welcome: Is the Church Colour-Blind

View page
Author

Thomas Joseph Holmes

ISBN #

0551006714

Ashes for Breakfast

View page
Author

Thomas Joseph Holmes

ISBN #

0817004440

Us Patents

Friction And Stiction Compensation For Spacecraft Attitude Control

View page
US Patent:
6517029, Feb 11, 2003
Filed:
Sep 13, 2000
Appl. No.:
09/660749
Inventors:
Thomas J. Holmes - Portola Valley CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
B64G 124
US Classification:
244164, 244165, 701 13
Abstract:
A spacecraft attitude control system that enables friction and stiction compensation for attitude control of a spacecraft using at least one reaction wheels that can spin through zero rpm without degradation in pointing. The system removes nuisance disturbances relating to friction or stiction that detract from the ability of the system to maintain or change spacecraft attitude. It can remove these effects before they are sensed by the systems attitude control sensors. A friction or stiction compensation buffer is arranged between the spacecraft attitude control subsystem and the torque actuators for the at least one reaction wheel. Since the compensation is localized to each wheel, it is possible to optionally: control wheel operating speeds to safe levels, provide wheel failure flags, provide accurate wheel tracking at slow or zero wheel speeds and provide full access to the wheel torques.

Transient-Free Gain Switching Within Error Threshold

View page
US Patent:
59496754, Sep 7, 1999
Filed:
Nov 1, 1996
Appl. No.:
8/742854
Inventors:
Thomas Joseph Holmes - Portola Valley CA
David L. Cielaszyk - Sunnyvale CA
David J. Wirthman - Mountain View CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
G05B 1302
US Classification:
364157
Abstract:
For a switching of a magnitude of system gain in the driving of a load by a control system, a method of inhibiting formation of switching transients has a step of distinguishing between an estimate of a plant state, such as the attitude of a spacecraft, and an integral control state which allows the control system to provide actuation in response to long term disturbances, such as solar pressure, in operation of the system. In the case of a feedback configuration to the system with controller in a forward branch and an estimator in a feedback branch, a loop error signal serves to drive an actuator of the load via the controller. The method includes a further step of evaluating a portion of a controller input signal which is exclusive of an integral control state and which comprises a difference between a desired state and an estimate of the plant state. The evaluation step enables observation of an occurrence of a magnitude of the difference which falls within a range of values satisfying a criteria of minimal effect on the actuator. There is a further step of switching a value of the gain during the occurrence.

Thruster On Time Signaling With Flexure Compensation Avoidance

View page
US Patent:
61253103, Sep 26, 2000
Filed:
Jul 18, 1997
Appl. No.:
8/896967
Inventors:
Thomas J. Holmes - Portola Valley CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
B64G 124
G05D 320
US Classification:
701 4
Abstract:
A system and process is described for maintaining the attitude of a space craft to compensate for external disturbances. The on board computer generates a thruster on time signal derived from a comparison of estimated adjusted attitude based substantially on rigid body assumptions which to do not take into consideration the flexing reactions of on board flexible components.

Thruster Control Of Yaw Without Yaw Measurements

View page
US Patent:
57526753, May 19, 1998
Filed:
Jul 3, 1995
Appl. No.:
8/498657
Inventors:
Thomas Joseph Holmes - Portola Valley CA
Peter Timothy Gauthier - Mountain View CA
John S. Higham - Mountain View CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
B64G 132
B64G 136
B64G 138
US Classification:
244168
Abstract:
An automatic, on-board system for orbiting spacecraft that controls yaw excursions caused by solar torques and thruster firings, which system combines inputs indicative of roll and yaw momentum increases and inputs containing information comprising the unbiased roll error from the earth sensor, yaw momentum measured from the wheel speeds, and commanded yaw momentum output from the wheel controller, and produces therefrom output signals indicative of the yaw estimate and the yaw momentum estimate. These output signals are combined and processed in a controller with a mimimum yaw error and roll thrust yaw controller gain and a miminmum yaw error and roll thrust yaw momentum controller gain, and a signal is produced therefrom for commanding roll thruster firings to change roll momentum, and, in turn, control yaw attitude and yaw excursions.

Spacecraft Control System With A Trihedral Momentum Bias Wheel Configuration

View page
US Patent:
58268294, Oct 27, 1998
Filed:
Jul 15, 1996
Appl. No.:
8/679575
Inventors:
Thomas Joseph Holmes - Portola Valley CA
Assignee:
Space Systems/Loral Inc. - Palo Alto CA
International Classification:
B64G 128
US Classification:
244165
Abstract:
An active attitude control system for a spacecraft having first, second, and third mutually perpendicular axes utilizes four flywheels, at a minimum, which can selectively provide options of fully redundant momentum bias, 3/4 redundant momentum bias, or fully redundant zero momentum bias. A plurality of reaction wheels are mounted on the spacecraft and rotatable on spin axes in a fixed configuration for together maintaining full three-axis control of the spacecraft to a predetermined attitude. A momentum wheel is also rotatable on the spacecraft about the first axis for maintaining gyroscopic stiffness. In the event of a failure of the momentum wheel, the reaction wheels may have a combined angular momentum sufficient to maintain the gyroscopic stiffness lost by the failure of the momentum wheel while maintaining full three-axis control of the spacecraft to a predetermined attitude. In one embodiment, the reaction wheels are mounted in a fixed trihedral configuration, a first reaction wheel being rotatable about a spin axis which lies in a plane of the first and second axes, and second and third reaction wheels being rotatable about spin axes which lie in a plane of the first axis and are oblique to the second and third axes.

Satellite Stabilization System

View page
US Patent:
56180128, Apr 8, 1997
Filed:
Jan 12, 1995
Appl. No.:
8/371821
Inventors:
John A. Lehner - Sunnyvale CA
Thomas Holmes - Portola Valley CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
B64G 124
US Classification:
244168
Abstract:
A satellite stabilization system compensates for the destabilizing torque introduced by solar radiation pressure by the emplacement of tabs of material angled relative to the back surfaces of the antenna reflectors to intercept solar rays. The material of the tabs interacts with the solar radiation in substantially the same manner as the interaction of the material on the back surface of each antenna reflector to produce a radiation pressure and consequential increment in a torque about an axis of the satellite. Each of the tabs is constructed in the manner of a plate or disk, and is attached by means of a spring mount to the back surface of one of the reflectors. The reflectors are angled relative to each other, as well as to a body of the satellite which holds feeds for illuminating the reflectors, for directing beams of radiation from the feeds towards the earth. Due to the angulation of the reflectors to each other, the total solar energy incident upon a pair of of the reflectors is generally unequal, this resulting in a net torque from the solar radiation pressure which tends to rotate the satellite. By virtue of the angulation of the tabs relative to the reflectors, an increased amount of solar radiation is received by the reflector which is angled away from the sun's rays, thereby to equalize the torque from both of the reflectors.

Onboard Attitude Control Using Reaction Wheels

View page
US Patent:
62859285, Sep 4, 2001
Filed:
Jan 6, 2000
Appl. No.:
9/478787
Inventors:
Scott W. Tilley - Belmont CA
Thomas J. Holmes - Portola Valley CA
Keith J. Reckdahl - Palo Alto CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
B64G 129
US Classification:
701 13
Abstract:
An onboard attitude control system is constructed to utilize a four reaction wheel system having a reference axis, wherein at least three of the reaction wheel spin axes are oriented obliquely to the reference axis. Current attitude is estimated based on uploaded orbital data, onboard sensed earth and sun position data, and attitude data sensed by a three axes gyroscope system. Current attitude is compared to mission attitude to calculate an error which is transformed to a trihedral axes adjustment command to actuate the reaction wheel system.

Thruster Optimized Pair Selection

View page
US Patent:
60526300, Apr 18, 2000
Filed:
Dec 17, 1996
Appl. No.:
8/768214
Inventors:
Thomas J. Holmes - Portola Valley CA
Christopher R. Purvis - Menlo Park CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
B64G 124
B64G 126
US Classification:
701 13
Abstract:
A method for controlling the direction of a spacecraft of the type having a controller for calculating thrust forces comprises a plurality of thrusters disposed on said spacecraft in a spaced relationship relative to one another and aligning and locating each of said plurality of thrusters at a predetermined angle on said spacecraft relative to first, second and third orthogonally oriented axes such that the firing of any given pair of thrusters produces a torque about one of said spacecraft axes; and firing of all of said plurality of said thrusters in equal amounts at one time to cause the spacecraft to move in a linear manner along one of said three orthognally disposed axes.
Control profile
Thomas W Holmes from Napa, CA, age ~74 Get Report