DR. ROBERT DODD, M.D., PH.D.
Medical Practice in Palo Alto, CA
License number
California A69623
Category
Medical Practice
Type
Neurological Surgery
Address
Address
300 Pasteur Dr Edwards Bldg., Palo Alto, CA 94305
Phone
(650) 725-5566
Organization information
See more information about ROBERT DODD at bizstanding.comRobert Dodd MD,PHD
300 Pasteur Dr, Stanford, CA 94305
Industry:
Neurosurgeon
Phone:
(650) 725-5566 (Phone)
Robert Louis Dodd
Professional information
Dr. Robert Dodd - MD (Doctor of Medicine)
Hospitals:
300 Pasteur Dr STE A301, Stanford 94305
Stanford Hospital and Clinics
300 Pasteur Dr, Stanford 94305
300 Pasteur Dr STE A301, Stanford 94305
Stanford Hospital and Clinics
300 Pasteur Dr, Stanford 94305
Stanford Hospital and Clinics
300 Pasteur Dr, Stanford 94305
300 Pasteur Dr STE A301, Stanford 94305
Stanford Hospital and Clinics
300 Pasteur Dr, Stanford 94305
Education:
Medical Schools
Stanford University School Of Medicine
Graduated: 1998
Stanford University School Of Medicine
Graduated: 1998
Robert Dodd, Stanford CA
Specialties:
Surgery, Neurological Surgery, Diagnostic Radiology
Work:
Stanford University
300 Pasteur Dr, Stanford, CA 94305 Stanford University
300 Pasteur Dr, Palo Alto, CA 94304
300 Pasteur Dr, Stanford, CA 94305 Stanford University
300 Pasteur Dr, Palo Alto, CA 94304
Education:
Stanford University (1998)
Robert Louis Dodd, Stanford CA
Specialties:
Neurosurgeon
Address:
300 Pasteur Dr, Stanford, CA 94305
Dual Antenna Null Elimination
US Patent:
5923292, Jul 13, 1999
Filed:
Jul 11, 1997
Appl. No.:
8/891484
Inventors:
Robert W. Dodd - Palo Alto CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
G01S 316, H04B 7185, H01Q 322
US Classification:
342383
Abstract:
RF signal nulling and loss of RF lock (i. e. , loss of a communications or command link) is resolved by changing the phase of signals derived from first and second (+Z and -Z) antennas so that they add in phase instead of canceling. This is accomplished automatically by using a computer or processor to measure the RF signal level output by a receiver and change the phase of the incoming signal using a phase shifter to achieve the highest level. A squelch circuit in the receiver is used to determine the maximum obtainable RF signal level. The squelch level is compared in a computer to a threshold when the system looks for a higher squelch level. The phase of the phase shifter is changed using a computer to maximize the received signal level. A feedback loop from the receiver through the computer to the phase shifter provides a path to shift the phase of the incoming RF signal in one of the paths so the respective signals add instead of cancel, which eliminates the signal nulling problem.
Software Select And Test
US Patent:
6018703, Jan 25, 2000
Filed:
Jun 18, 1998
Appl. No.:
9/099154
Inventors:
Robert W. Dodd - Palo Alto CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
G05B 2302
US Classification:
702113
Abstract:
A software-controlled select and test system for use with a spacecraft. The system reduces the assembly, integration, test time and improves performance of the payload and spacecraft by optimizing the performance using standardized algorithms. The system also reduces the DC power required by the spacecraft, and the thermal dissipation, battery size, solar array size and mass of the spacecraft. This is achieved by optimizing traveling wave tube amplifiers for each channel instead of meeting minimum power requirement over the entire range, wherein most channels have excess power. A serial interface adapter performs the optimization functions via software.
Software Select And Test
US Patent:
5781456, Jul 14, 1998
Filed:
Jul 11, 1997
Appl. No.:
8/891491
Inventors:
Robert W. Dodd - Palo Alto CA
Assignee:
Space Systems/Loral, Inc. - Palo Alto CA
International Classification:
G05B 2302
US Classification:
364579
Abstract:
A software-controlled select and test system for use with a spacecraft. The system reduces the assembly, integration, test time and improves performance of the payload and spacecraft by optimizing the performance using standardized algorithms. The system also reduces the DC power required by the spacecraft, and the thermal dissipation, battery size, solar array size and mass of the spacecraft. This is achieved by optimizing traveling wave tube amplifiers for each channel instead of meeting minimum power requirement over the entire range, wherein most channels have excess power. A serial interface adapter performs the optimization functions via software.