Patents Represented by Attorney Robert D. Marchant
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Patent number: 5802255Abstract: A system and method provides for the creation of a highly graphical expert system without the need for programming in code. An expert system is created by initially building a data interface, defining appropriate Mission, User-Defined, Inferred, and externally-generated GenSAA (EGG) data variables whose data values will be updated and input into the expert system. Next, rules of the expert system are created by building appropriate conditions of the rules which must be satisfied and then by building appropriate actions of rules which are to be executed upon corresponding conditions being satisfied. Finally, an appropriate user interface is built which can be highly graphical in nature and which can include appropriate message display and/or modification of display characteristics of a graphical display object, to visually alert a user of the expert system of varying data values, upon conditions of a created rule being satisfied.Type: GrantFiled: June 23, 1995Date of Patent: September 1, 1998Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Peter M. Hughes, Edward C. Luczak
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Patent number: 5726581Abstract: A capacitive type proximity sensor having improved range and sensitivity between a surface of arbitrary shape and an intruding object in the vicinity of the surface having one or more outer conductors on the surface which serve as capacitive sensing elements shaped to conform to the underlying surface of a machine. Each sensing element is backed by a reflector driven at the same voltage and in phase with the corresponding capacitive sensing element. Each reflector, in turn, serves to reflect the electric field lines of the capacitive sensing element away from the surface of the machine on which the sensor is mounted so as to enhance the component constituted by the capacitance between the sensing element and an intruding object as a fraction of the total capacitance between the sensing element and ground.Type: GrantFiled: March 8, 1996Date of Patent: March 10, 1998Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 5687255Abstract: A pre-coding method and device for improving data compression performance by removing correlation between a first original data set and a second original data set, each having M members, respectively. The pre-coding method produces a compression-efficiency-enhancing double-difference data set. The method and device produce a double-difference data set, i.e., an adjacent-delta calculation performed on a cross-delta data set or a cross-delta calculation performed on two adjacent-delta data sets, from either one of (1) two adjacent spectral bands coming from two discrete sources, respectively, or (2) two time-shifted data sets coming from a single source. The resulting double-difference data set is then coded using either a distortionless data encoding scheme (entropy encoding) or a lossy data compression scheme. Also, a post-decoding method and device for recovering a second original data set having been represented by such a double-difference data set.Type: GrantFiled: January 3, 1995Date of Patent: November 11, 1997Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Pen-Shu Yeh
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Patent number: 5576663Abstract: A method and apparatus for increasing the bandwidth of an operational amplifier and including a capacitor being connected across the inverting and non-inverting inputs of the operational amplifier and further including a feedback circuit connected from the output to one of the inputs, the inverting input, and wherein the value of the capacitance is selected such that the time constant of an RC network including the capacitance and the feedback circuit impedance is proportional to the inverse of the product of the closed loop gain and a factor .beta. which equates the absolute value of the gain at two different frequencies.Type: GrantFiled: March 24, 1995Date of Patent: November 19, 1996Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: Leonard L. Kleinberg
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Patent number: 5566139Abstract: A time interval unit which operates in accordance with electronic sampling techniques and employing a pair of identical sampling interpolators which are respectively triggered at the start and stop of the time interval to be measured. Each time interval unit includes a GHz frequency sinusoidal clock signal generator and a time counter in the form of a pulse counter and a pair of sampling type interpolators which are respectively triggered on in response to a start and a stop signal. When triggered, each interpolator samples the instantaneous amplitude of the in-phase(x) and quadrature(y) components of the sinusoidal clock signal. From the samples of the x and y components and the pulse counter's result, the elapsed time between two events is computed to a psec accuracy.Type: GrantFiled: September 20, 1993Date of Patent: October 15, 1996Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: James B. Abshire
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Patent number: 5521515Abstract: A capaciflector sensor system scanned in frequency is used to detect the permittivity of the material of an object being sensed. A capaciflector sensor element, coupled to current-measuring voltage follower circuitry, is driven by a frequency swept oscillator and generates an output which corresponds to capacity as a function of the input frequency. This swept frequency information is fed into apparatus e.g. a digital computer for comparing the shape of the capacitance vs. frequency curve against characteristic capacitor vs. frequency curves for a variety of different materials which are stored, for example, in a digital memory of the computer or a database. Using a technique of pattern matching, a determination is made as to the identification of the material. Also, when desirable, the distance between the sensor and the object can be determined.Type: GrantFiled: February 17, 1995Date of Patent: May 28, 1996Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Charles E. Campbell
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Patent number: 5515001Abstract: An operational amplifier connected in series with a load and a current-measuring impedance and having at least two input ports and an output port, the output port of the operational amplifier further being directly connected to current-measuring impedance, with one of the input ports being coupled to the current input source to be measured, and the other input port being connected to a feedback loop coupled from the output side of the current-measuring impedance. The voltage across the current-measuring impedance which comprises a resistor is thereafter sensed, amplified and conditioned to provide a voltage which is proportional to the load current and accordingly a measure of the current input from the current source being measured. Such a current-measuring circuit can be used in connection with an inverter, a current-measuring amplifier, a current-measuring precision diode, a current integrator, and a current-measuring bridge.Type: GrantFiled: January 31, 1994Date of Patent: May 7, 1996Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 5482144Abstract: A torque coupling sprag system which provides contact between the sides of at least one groove and at least two contact surfaces angled with respect to the central axial direction of at least one rotatable 3-D sprag member located between a drive member and a reaction member. The surface contacts between the members include various combinations of surface segments arranged in a predetermined manner to define a desired configuration. The contact radius of the 3-D sprag member is significantly larger than its rolling radius; however, radii can be varied in size and shape independently of each other, particularly the contact radius.Type: GrantFiled: July 27, 1994Date of Patent: January 9, 1996Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 5483058Abstract: A device for position encoding of a rotating shaft in which a polygonal mirror having a number of facets is mounted to the shaft and a monochromatic light beam is directed towards the facets. The facets of the polygonal mirror direct the light beam to a stand-alone low line density diffraction grating to diffract the monochromatic light beam into a number of diffracted light beams such that a number of light spots are created on a linear array detector. An analog-to-digital converter is connected to the linear array detector for reading the position of the spots on the linear array detector means. A microprocessor with memory is connected to the analog-to-digital converter to hold and manipulate the data provided by the analog-to-digital converter on the position of the spots and to compute the position of the shaft based upon the data from the analog-to-digital converter.Type: GrantFiled: October 18, 1993Date of Patent: January 9, 1996Assignee: The United States of America as represented by the Administrator, National Aeronautics & Space AdministrationInventor: Douglas B. Leviton
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Patent number: 5451294Abstract: An elongated fixture handle member is connected to a fixture body member with both members having interconnecting longitudinal central axial bores for the passage of an optical cable therethrough. The axial bore of the fixture body member, however, terminates in a shoulder stop for the outer end of a jacket of the optical cable covering both an optical fiber and a coating therefor, with an axial bore of reduced diameter continuing from the shoulder stop forward for a predetermined desired length to the outer end of the fixture body member. A subsequent insertion of the fixture body member including the above optical fiber elements into a chemical stripping solution results in a softening of the exposed external coating thereat which permits easy removal thereof from the optical fiber while leaving a desired length coated fiber intact within the fixture body member.Type: GrantFiled: May 31, 1994Date of Patent: September 19, 1995Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John R. Kolasinski, Alexander M. Coleman
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Patent number: 5447403Abstract: An anatomically correct, humanlike, mechanical arm and hand is provided that an operator can control to perform with the dexterity and compliance of a human hand. Being humanlike and robotic enhances the device's control and gripper dexterity. Control of the movement of the arm and hand is performed or guided by a "teachglove" worn by the operator. As he or she performs some hand manipulation, a controller stores signals from sensors on the exoskeleton. The sensors monitor the operator's finger-joint movement positions. These values are later translated into actuator control signals for servomotors, eventually duplicating the operator's movement.Type: GrantFiled: May 28, 1993Date of Patent: September 5, 1995Inventor: Charles D. Engler, Jr.
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Patent number: 5448642Abstract: A method of lossless data compression for efficient coding of an electronic signal of information sources of very low information rate is disclosed. In this method, S represents a non-negative source symbol set, {s.sub.0, s.sub.1, s.sub.2, . . . s.sub.N-1 } of N symbols with s.sub.i =i. The difference between binary digital data is mapped into symbol set S. Consecutive symbols in symbol set S are then paired into a new symbol set .GAMMA. which defines a non-negative symbol set containing the symbols {.gamma..sub.m } obtained as the extension of the original symbol set S. These pairs are then mapped into a comma code which is defined as a coding scheme in which every codeword is terminated with the same comma pattern, such as a 1. This allows a direct coding and decoding of the n-bit positive integer binary digital data differences without the use of codebooks.Type: GrantFiled: February 14, 1994Date of Patent: September 5, 1995Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Pen-Shu Yeh
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Patent number: 5418709Abstract: A pulse-width modulated DC-to-DC power converter including a first inductor, i.e. a transformer or an equivalent fixed inductor equal to the inductance of the secondary winding of the transformer, coupled across a source of DC input voltage via a transistor switch which is rendered alternately conductive (ON) and non-conductive (OFF) in accordance with a signal from a feedback control circuit. A first capacitor capacitively couples one side of the first inductor to a second inductor which is connected to a second capacitor which is coupled to the other side of the first inductor. A circuit load shunts the second capacitor. A semi-conductor diode is additionally coupled from a common circuit connection between the first capacitor and the second inductor to the other side of the first inductor.Type: GrantFiled: March 24, 1993Date of Patent: May 23, 1995Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Alan T. Lukemire
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Patent number: 5399993Abstract: High input impedance amplifiers are provided which reduce the input impedance solely to a capacitive reactance, or, in a somewhat more complex design, provides an extremely high essentially infinite, capacitive reactance. In one embodiment, where the input impedance is reduced in essence, to solely a capacitive reactance, an operational amplifier in a follower configuration is driven at its non-inverting input and a resistor with a predetermined magnitude is connected between the inverting and non-inverting inputs. A second embodiment eliminates the capacitance from the input by adding a second stage to the first embodiment. The second stage is a second operational amplifier in a non-inverting gain-stage configuration where the output of the first follower stage drives the non-inverting input of the second stage and the output of the second stage is fed back to the non-inverting input of the first stage through a capacitor of a predetermined magnitude.Type: GrantFiled: August 26, 1993Date of Patent: March 21, 1995Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Leonard L. Kleinberg
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Patent number: 5396073Abstract: A circuit for high resolution decoding of multi-anode microchannel array detectors consisting of input registers accepting transient inputs from the anode array, anode encoding logic circuits connected to the input registers, midpoint pipeline registers connected to the anode encoding logic circuits and pixel decoding logic circuits connected to the midpoint pipeline registers. A high resolution algorithm circuit operates in parallel with the pixel decoding logic circuit and computes a high resolution least significant bit to enhance the multi-anode microchannel array detector's spatial resolution by halving the pixel size and doubling the number of pixels in each axis of the anode array. A multiplexer is connected to the pixel decoding logic circuit and allows a user selectable pixel address output according to the actual multi-anode microchannel array detector anode array size.Type: GrantFiled: May 7, 1992Date of Patent: March 7, 1995Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: David B. Kasle
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Patent number: 5373245Abstract: A capacitive type proximity sensor having improved range and sensitivity between a surface and an intruding object in the vicinity of the surface having a voltage source, a number of outer electrical conductors on the surface with each forming one electrode of a number of sensor capacitors, the other electrode for each sensor capacitor being the object. The outer conductors are made from thin sheets of conductive material covered with insulation. An intermediate electrical conductor is located between the outer conductors and the surface and is of a size larger than the outer conductors to act as a shield for reducing the parasitic capacitance between the outer conductors and the surface. The intermediate conductor is also made from a thin sheet of conductive material covered with insulation.Type: GrantFiled: July 12, 1993Date of Patent: December 13, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 5373263Abstract: An electron beam microwave device having an evacuated interaction chamber to which are coupled a resonant cavity which has an opening between the resonant cavity and the evacuated interaction chamber and an electron gun which causes a narrow beam of electrons to traverse the evacuated interaction chamber. The device also contains a mechanism for feeding back a microwave electromagnetic field from the resonant cavity to the evacuated interaction chamber in such a way as to modulate the direction of propagation of the electron beam, thereby further amplifying the microwave electromagnetic field. Furthermore, provision is made for coupling the electromagnetic field out of the electron beam microwave device.Type: GrantFiled: March 22, 1993Date of Patent: December 13, 1994Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: Lawrence E. Wharton
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Patent number: 5363288Abstract: A high voltage power supply in a dc--dc converter configuration includes a pre-regulator which filters and regulates the dc input and drives an oscillator which applies, in turn, a low voltage ac signal to the low side of a step-up high voltage transformer. The high voltage side of the transformer drives a voltage multiplier which provides a stepped up dc voltage to an output filter. The output voltage is sensed by a feedback network which then controls a regulator. Both the input and output of the regulator are on the high voltage side, avoiding isolation problems. The regulator furnishes a portion of the drive to the voltage multiplier, avoiding having a regulator in series with the load with its attendant, relatively high power losses. This power supply is highly regulated, has low power consumption, a low parts count and may be manufactured at low cost. The power supply has a programmability feature that allows for the selection of a large range of output voltages.Type: GrantFiled: April 1, 1993Date of Patent: November 8, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Karen D. Castell, Arthur P. Ruitberg
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Patent number: 5358460Abstract: A plurality of flexible cylindrical members, termed flex-gears and having gear tooth type perimeters are located in an annular space between two concentric rotating gear members, one an inner gear member and the other an outer ring gear member, both of which have mutually facing toothed surfaces which engage the flex-gears. The flex-gears rotate and orbit around the annular space as planetary gears when the inner and outer gear members rotate with respect to one another. Pairs of these elements located in two mutually parallel planes and separated by insulators provide two electrical conductor paths across which an electrical signal source, AC or DC, can be connected and coupled to an electrical device. Alternatively, one set of elements including outer gears segmented into mutually insulated semicircles and inner gears segmented into mutually insulated quadrants can be used.Type: GrantFiled: January 25, 1993Date of Patent: October 25, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 5357371Abstract: A laser retroreflector array is provided having an array of cat-eye retroreflectors each with an image forming objective through which the laser beam passes and a partial mirror at the focal plane of the image forming objective. By using the cat-eye retroreflectors to reflect the laser beam, the field of view can be angularly limited so that only one retroreflector in the array at a time reflects the laser beam.Type: GrantFiled: September 22, 1992Date of Patent: October 18, 1994Assignee: The United States of America as represented by the Administrator, National Aeronautics & Space AdministrationInventor: Peter O. Minott