Thomas C Holmes

age ~73

from Highlands, NC

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Also known as:

Thomas Florence Holmes
Tom C Holmes

Connected to:

Thomas Holmes Phones & Addresses

Highlands, NC
Atlanta, GA
Hamilton, GA
San Francisco, CA
Ross, CA

Wikipedia References

Thomas Holmes (Executive)

Thomas Holmes (Politician)

Real Estate Brokers

Thomas Holmes, Florida Agent

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Specialties:

Residential sales
Luxury homes

Work:

Champagne & Parisi Real Estate
(561)7063203 (Phone)
License #30673245

Client type:

Home Buyers
Home Sellers

Property type:

Single Family Home
Condo/Townhome

Languages:

English

Name / Title

Company / Classification

Phones & Addresses

Mr. Thomas Holmes Jr.
Owner

Cackalak Clothing Co.
Internet Shopping Services

PO BOX, 12061, Columbia, SC 29211
(888)5220781

Thomas Holmes
COO

Thomas L. Holmes
Offices of Bank Holding Companies

3835 Killkenny Ct, Alpharetta, GA 30023

Thomas Dale Holmes

Headwaters Realty
Real Estate Agents and Managers

11937 State Hwy 197 N, Clarkesville, GA 30523

Thomas Holmes
Vice-President

Container Management Services LLC
Mfg Metal Barrels/Pails

21301 Cloud Way, Hayward, CA 94545
(510)2716200

Thomas Holmes
Principal

New Mercies Pentecostal Temple, Inc. Church of God In Christ
Religious Organization

230 Shiver Blvd, Porterdale, GA 30016

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 M. Holmes
Neurology, Medical Doctor

Neurological Associates Marietta PC
Neurologist

780 Canton Rd NE, Marietta, GA 30060
(770)4223602

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

Vehicle Records

Thomas Holmes
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Address:

3811 Clb Dr NE, Atlanta, GA 30319
Phone:

(404)2373982
VIN:

2HNYD28397H511188
Make:

ACURA
Model:

MDX
Year:

2007

Medicine Doctors

Dr. Thomas M Holmes, Marietta GA - MD (Doctor of Medicine)

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Specialties:

Clinical Neurophysiology
Neuromusculoskeletal Medicine

Address:

Marietta Neurology/Headache Center
780 Canton Rd Ne Suite 400, Marietta, GA 30060
(770)4223602 (Phone)

Certifications:

Clinical Neurophysiology, 2007
Neurology, 2006

Awards:

Healthgrades Honor Roll

Languages:

English
Russian

Hospitals:

Marietta Neurology/Headache Center
780 Canton Rd Ne Suite 400, Marietta, GA 30060

Wellstar Kennestone Hospital
677 Church Street North East, Marietta, GA 30060

Education:

Medical School
Duke University School Of Medicine
Graduated: 2001

Thomas M. Holmes

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Specialties:

Neurology

Work:

WellStar Medical GroupMarietta Neurology & Headache Center
780 Canton Rd NE STE 400, Marietta, GA 30060
(770)4223602 (phone), (770)4216115 (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 G. Holmes

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Specialties:

Internal Medicine

Work:

Advocate Medical Group
1775 Ballard Rd, Park Ridge, IL 60068
(847)3182500 (phone), (847)3182966 (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 J. Holmes

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Specialties:

Emergency Medicine

Work:

Middlesex Hospital Emergency
28 Cres St, Middletown, CT 06457
(860)3588000 (phone), (860)3588010 (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.

Thomas Michael Holmes, Marietta GA

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Specialties:

Neurology
Clinical Neurophysiology

Work:

Marietta Neurological Associates
780 Canton Rd NE, Marietta, GA 30060

Education:

Duke University(2001)
Jackson Memorial Hospital (2002) *
Massachusetts General Hospital (2005) *
Brigham and Women's Hospital (2005) *

Thomas M Holmes, Marietta GA

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Specialties:

Neurologist

Address:

780 Canton Rd Ne, Marietta, GA 30060

Pages
174

ISBN #
8

Us Patents

Friction And Stiction Compensation For Spacecraft Attitude Control
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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
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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
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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
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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
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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.

Onboard Attitude Control Using Reaction Wheels
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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
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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.

Transient Free Actuator Switching
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US Patent:

61389528, Oct 31, 2000
Filed:

Jun 11, 1999
Appl. No.:

9/330404
Inventors:

Thomas J. Holmes - Portola Valley CA
Assignee:

Space Systems/Loral, Inc. - Palo Alto CA
International Classification:

B64G 124
US Classification:

244164
Abstract:

An automatic apparatus and method that is used to switch actuators, such as momentum wheels, used on a spacecraft without impacting the pointing performance of the spacecraft. The apparatus and method allows an actuator to be automatically deactivated without affecting spacecraft performance such as is caused by a failed actuator. A plurality of local actuator controllers are respectively coupled to a plurality of actuators. A system controller is coupled to the plurality of local controllers and implements a control algorithm corresponding to the present method that determines forces/torques for each of the actuators and outputs force/torque commands to each of the actuators to control the pointing direction of the spacecraft. This is achieved by estimating the drag exerted by or integral control signal produced by each actuator to determine if it is approaching failure. In the event of failure, a backup actuator is activated, the failing actuator is shut down, and the forces/torques exerted by the remaining actuators are adjusted in an amount corresponding to the force/torque exerted by the failing actuator.

Lawyers & Attorneys

Thomas Holmes - Lawyer

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Office:

Thomas J. Homes, Esq.

ISLN:

906402557

Admitted:

1975

University:

Boston College, B.A., 1972

Law School:

Suffolk University, J.D., 1975

Thomas Holmes - Lawyer

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ISLN:

910610542

Admitted:

1993

University:

Rutgers Newark

Thomas Holmes - Lawyer

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Specialties:

Labor & Employment
School Law
Education & School Law

ISLN:

916637536

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Locality:

J-Ville, Florida

Gender:

Male

Birthday:

1952

Thomas holmes

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Locality:

b-lo all day nigga!!!!!!

Gender:

Male

Birthday:

1943

Plaxo

Thomas Holmes

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GM Machine llc

Thomas Holmes

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self employed

News

Creative Arts Emmys 2018: Winners List

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Thomas Holmes, Production Mixer Mikael Stewart, Production Mixer John Harris, Broadcast Music Mixer Eric Schilling, Broadcast Music Mixer Ron Reaves, Front of House Music Mixer Thomas Pesa, Stage Foldback Mixer Simon Welch, Stage Foldback Mixer Eric Johnston, Playback Music Mixer Pablo Munguia, Pro
Date: Sep 08, 2018
Category: Headlines
Source: Google

Creative Arts Emmy Winners: Updated List

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Sound Mixing For a Variety Special Series or Special (tie)Josh Morton, Thomas Holmes, Mikael Stewart, Eric Schilling, John Harris, Ron Reaves, Thomas Pesa, Michael Parker, Eric Johnston, Pablo Munguia, Bob LaMasney (59th Grammy Awards)Al Centrella, Susan Pelino, Jay Vicari, Dave Natale, Erik Von
Date: Sep 09, 2017
Category: Entertainment
Source: Google

Barton County getting healthier

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Approved the appointment of City of Great Bend assistant sanitarian Thomas Holmes to be a representative of the city on the Solid Waste Planning Committee. Per Kansas statutes, Barton County is required to maintain a Solid Waste Planning Committee to develop and perform an annual review of the Sol
Date: Mar 21, 2016
Category: Health
Source: Google

Sen. Johnny Isakson announces Parkinson's disease diagnosis

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include a slowed, shuffling gait. Although there is no cure for Parkinsons, there are treatment options to help manage the symptoms, which progress over time. According to Isaksons doctor, Thomas Holmes, the senators regiment includes physical therapy, exercise, and two medications.
Date: Jun 10, 2015
Category: U.S.
Source: Google

Sen. Isakson has Parkinson's; will run for new term

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The 70-year-old lawmaker announced his diagnosis in a statement accompanied by a note from his doctor that described the current symptoms as mild. Dr. Thomas Holmes wrote that Isakson is fully capable of running again and serving another term.
Date: Jun 10, 2015
Category: Health
Source: Google

Sen. Isakson has Parkinson's disease

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Isakson's office released a statement from his neurologist, Dr. Thomas Holmes, who said the senator is in stage 1.5 of five accepted stages of Parkinson's disease. His symptoms include a stiff left arm and a shuffling gait.
Date: Jun 10, 2015
Category: Health
Source: Google