Abstract: A high capacity radar plot display with low CPU loading. The display includes a display process (42) which controls a graphics window server (46) to render symbols on a display console by a "walking worm" animation. The current symbol plot as well as several symbol plot histories are sequentially displayed to render the animation. A plurality of color maps defining the colors of the current and plot histories are defined, with a clear color map to clear the display. The clear color map includes black (nonvisible) color for all the current and plot histories. The color map for the oldest plot history has a visible color assigned to the oldest history plot, with all other plot histories and the current plot still in black. Successive color maps for the remaining plot histories and the current plot, from the next oldest to the current plot, have progressively more plot histories in a visible color.

Abstract: Contaminants are cleaned from the surface of a body in space by generating a substantially space-charge neutral reactive plasma, directing the plasma onto the contaminated surface at an energy below the surface sputtering energy (typically 20 eV), and reacting the plasma with the contaminants to remove them. A helicon wave plasma source is made light weight and compact enough for spacecraft use, with a plasma energy low enough to avoid damaging optical surfaces, by using permanent magnets to establish a static axial magnetic field, and a simple but novel rf antenna design. The antenna consists of a pair of spaced conductive rings which extend around the plasma tube, with conductive base and rf feed bars extending between the rings on diametrically opposite sides. The feed bar is interrupted to provide an rf input on opposite sides of the interruption. The antenna is preferably formed as an integral metal unit, with its rings rigidly supported by and integral with opposite ends of the base bar.

Abstract: A sensor is provided for detecting the presence of dielectric media, e.g., ice. The sensor includes a plurality of microstrip resonators which are positioned for electromagnetic coupling with a microstrip transmission line. The resonators produce amplitude minima in a radio-frequency signal that is carried over the transmission line. The resonance of the resonators changes in response to the addition of a dielectric coating. Each resonator can be configured with a different resonant frequency which serves as a signature that identifies the respective resonator's position. The sensor has a thin aerodynamic profile, can conform to nonplanar surfaces and its installation requires no intrusion into an aircraft skin.

Abstract: A high-speed flywheel includes a composite rim supported for rotation about a central axis which is perpendicular to the plane of the rim. The rim includes at least a pair of rim portions or regions of differing elastic modulus in the circumferential direction of the material forming the rim. Moreover, a radially outer portion of the rim has a higher elastic modulus in the circumferential direction, while a radially inner portion of the rim has a lower elastic modulus in the circumferential direction. This variation of circumferential elastic modulus is achieved by a selected radial variation of the angle of the fiber reinforcement material relative to the circumferential direction of the rim. A result is that the radially inner portion of the rim transfers radial force to the outer portion, with a resulting lower radial stress in the radially inner portion of the flywheel rim. An improved speed of operation and greater energy storage for the flywheel is achieved.

Abstract: A method and system of attitude steering and momentum management for a spacecraft suitable over a wide range of orbit altitude and inclination parameters and a similar wide range of mission steering profiles is provided. The system utilizes two active momentum wheels positioned with their spin axes nominally coaligned on the spacecraft pitch axis. Each wheel is pivoted by jackscrew type mechanisms which allow the angular momentum to be tilted (e.g. within the range 0-45.degree. from the nominal alignment with respect to the spacecraft body). The spacecraft control processor generates wheel torque commands for the wheel speed electronics and jackscrew drive commands for the platform assemblies in order to adjust the speed and amount of tilt of the momentum wheels. The invention provides a two-momentum wheel array that allows use of either momentum bias steering or large angle zero-momentum steering and accommodates multiple orbit geometries and varying degrees of attitude steering agility.

Abstract: A high-speed flywheel includes a composite rim supported for rotation about a central axis which is perpendicular to the plane of the rim. The rim includes at least a pair of rim portions or regions of differing elastic modulus in the circumferential direction of the material forming the rim. Moreover, a radially outer portion of the rim has a higher elastic modulus in the circumferential direction, while a radially inner portion of the rim has a lower elastic modulus in the circumferential direction. This variation of circumferential elastic modulus is achieved by a selected radial variation of the angle of the fiber reinforcement material relative to the circumferential direction of the rim. A result is that the radially inner portion of the rim transfers radial force to the outer portion, with a resulting lower radial stress in the radially inner portion of the flywheel rim. An improved speed of operation and greater energy storage for the flywheel is achieved.

Abstract: A long-term thermally stable cryostat (40). The cryostat (40) pre-cools an incoming high-pressure gas, converts it to a cold liquid, contains the liquid, and cools an item by allowing the liquid to acquire heat from the item and boil into an exhaust gas, while maintaining an absolute pressure in the container to reduce thermal noise due to altitude-induced pressure changes. In specific embodiments, the cryostat (40) includes a hollow mandrel (52) disposed within a cooling volume (64) mounted within a dewar vacuum area (58). Pre-cooling fins (44) spiral around the hollow mandrel (52) within the cooling volume (64) and circulate an incoming high-pressure gas around the mandrel (52). A flow restrictor (60) receives the incoming gas from the pre-cooling fins (44) and releases it into the cooling volume (64), thereby converting the incoming gas into a cold liquid which can acquire heat from the item and boil into an exhaust gas.

Abstract: Boresighting apparatus that includes a multispectral reflective collimator combined with an adjustable rhomboid reflector that allows boresighting of any wavelength sighting, pointing, aiming or rangefinding device disposed on a small arms weapon. The boresighting apparatus comprises a housing and a small arms weapon adapter for securing the housing to small arms weapons having different calibers. An illuminated or heated target is disposed in the housing for selectively providing an image of an illuminated or heated target pattern. A power source is coupled to the target for providing power to selectively illuminate or heat the target. An adjustment mechanism is provided for incrementally adjusting the optical location of the target and thus the location of the target pattern. A mirror, such as an off-axis parabolic mirror, is disposed to reflect the image of the illuminated or heated target pattern along a visual optical path.

Abstract: The invention is directed to the reduction of an electron beam transport problem during microwave generation in plasma-assisted microwave sources. A small, e.g., <200 gauss, secondary magnetic field is positioned in association with a slow-wave structure (SWS) of the sources to reduce the radial divergence of electron bunches in the sources' electron beams. The secondary magnetic field exerts radial forces on diverging electrons to supplement radial forces of a primary magnetic field and radial forces of an electrostatic field. The primary magnetic field is generated by electron movement in the electron beam and the electrostatic field is generated by ions which are created as the electron beam transits an ionizable gas in the plasma-assisted source. The addition of the secondary magnetic field can be implemented with a coil that is positioned to direct at least a portion of its magnetic field through a passage of the SWS.

Abstract: A number of program modules (32,34,36) are sequentially controlled by a procedural user interface (PUI) 38 and an operating system (40) to perform tasks. Transfer of files or other data entities between the modules (32,34,36) and a storage (13) is seamlessly integrated by a sequential information integration service (SIIS) (50). For reading a file from the storage (13), a the PUI 38 or the operating system (40) generates a read command including a filename designation which can include a pathname, complete filename or wildcard characters. The read command can also include one or more arguments such as a user or group access code and an error message to display if the required file is not found. In an automatic mode, the service (50) automatically selects the most recent file corresponding to the filename designation and arguments, or displays the error message if a file meeting these criteria is not found.

Abstract: An optical assembly (10) includes a first plurality of optical elements (14) providing the viewer a first field of view and a second plurality of optical elements (18) that, when moved into the optical path (16), provides the viewer with a second field of view. A support structure (36) for the second plurality of optical elements (18) includes a permanent magnet (64) that is disposed to cause a switch (66) located on the housing (12) of the optical assembly (10) to close. The changing of the position of the switch (66) results in a signal being provided to identify to the viewer which field of view is being presented by the assembly (10).

Abstract: An athermalized and achromatized optical system (10, 30) has a lens group (12, 32) focusing energy on a focal plane (14, 42). The lens group (12, 32) includes at least two optical elements (22, 24, 26, 34, 36) of different material and a diffractive optical element (28, 40). The system (10, 30) enables athermalization and achromatization of the optical system.

Abstract: A system and method that provides an electronic indication that unauthorized access has been gained to a system. The mechanisms used by the present invention cannot be forged, bypassed, or subverted. In fact, even persons authorized to access the environment cannot do so without leaving evidence. When an intrusion is detected, a random number is generated. This random number, referred to as an audit count, is then encrypted and stored, and a sequence number is incremented. To recover this information at a later time, a trusted individual inserts an external device containing a decryption key. The decryption key is extracted, and the encrypted audit count and sequence number are decrypted and displayed. Periodic verification that the audit count and sequence number have not changed provides assurance that access has not been gained to the system.

Abstract: An opto-electronic accelerometer and pressure sensor formed on a substrate are disclosed. The sensor includes a light source and a plurality of light detectors exposed on a semiconductor substrate. A cantilever beam extends over the substrate. The cantilever beam is positioned such that it reflects light from the light source as an applied force urges the cantilever beam to deflect relative to the plurality of light detectors. Acceleration or pressure can be determined by the slope change of the cantilever beam and is computed by taking the ratio of illumination between corresponding light detectors. In an alternative embodiment, the cantilever beam includes a proof mass. In a further embodiment, a pressure sensor is coupled with a linkage rod which is connected to the cantilever beam and then connected to a diaphragm which is displaced as a pressure is applied.

Abstract: A packaged electronic structure includes an electronic device, and a package to which the electronic device is affixed. At least a portion of the package is made of a composite material of aluminum nitride dispersed in aluminum. The composite material is preferably prepared by mixing powders of the aluminum nitride and aluminum, and thereafter pressing and sintering the mixture.

Abstract: A method of fabricating self-aligned static induction transistors is disclosed. The method comprises fabricating a silicon substrate having an active area. A guard ring is formed around the active area. Source and gate regions are formed, and a self-aligned relatively deep trench in accordance with the present invention is formed over the gate regions. This is achieved by forming an oxide layer, and forming a polysilicon layer on the oxide layer. A second oxide layer is formed on the polysilicon layer which is then masked by a self-aligning mask. Trenches are etched into the source and gate regions using the self-aligning mask and gate regions are formed at the bottom of the trenches. The transistors are then processed to completion by forming gate, source and drain regions.

Abstract: Processing methods and apparatus that process magnetometer data derived from an array of magnetometer sensors and outputs both the position and velocity of a magnetic dipole. In the method and apparatus, (a) a set of actual magnetic field measurements of a magnetic dipole is collected using the array of magnetic sensors. Then (b), a trajectory for the magnetic dipole is hypothesized. Then (c), a set of estimated magnetic field measurements is determined that would be formed by a magnetic dipole moving along the hypothesized trajectory. Then (d), the actual magnetic field measurements are compared with the estimated magnetic field measurements. Then (e), based on the comparison, a new trajectory for the magnetic dipole is hypothesized. Steps (c) through (e) are repeated until agreement between the actual magnetic field measurements and the estimated magnetic field measurements is deemed sufficiently close. The trajectory is displayed for viewing on a display.

Abstract: An ultrasound detection system that is relatively insensitive to rough workpiece surfaces, suppresses low frequency noise, and provides high sensitivity without the need for active stabilization. An optical probe beam is reflected and phase modulated by a workpiece surface that is being vibrated by ultrasound. A time-delay interferometer optically interferes the phase modulated probe beam with a time-delayed replica of itself. The optical interference generates optical interference fringes that move in accordance with the workpiece surface velocity. The interference fringes are detected by a non-steady-state photo-electromotive-force (NSS-photo-EMF) detector that generates an output signal when the frequency of fringe motion exceeds a predetermined threshold.

Abstract: A method and apparatus for enabling the use of optical techniques for temperature measurement of a semiconducting substrate coated with an optically opaque overlayer. A reflective mirror structure is inserted between the semiconducting substrate and the optically opaque overlayer. The reflective structure prevents the overlayer from absorbing light transmitted through the semiconducting substrate and instead reflects the light, thereby restoring the substrate front-surface reflectivity required for temperature measurement analysis by optical techniques such as absorption edge reflectance spectroscopy.

Abstract: A scanning detection system. The inventive system includes a detector arrangement for scanning a target surface over a predetermined angular range and providing a plurality of sampled signals in response thereto. The detector outputs are sampled and aggregated to provide a first output having a constant spatial resolution independent of the scan angle of the detector. The detector outputs are also aggregated to provide a second output having fine radiometric sensitivity. In a specific implementation, constant resolution is achieved by co-adding a variable number of adjacent detector samples where the number of adjacent samples co-added is dependent on the scan angle. Fine radiometric sensitivity is achieved by co-adding a fixed number of adjacent samples. Thus, dual capabilities of constant resolution and high sensitivity are achieved in a cost effective manner.