Digital devices development - Nine-channel autocorrelator and SDS 900 series computer interface logic
Nine-channel autocorrelator and SDS 900 computer interface logic
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Nine-channel autocorrelator and SDS 900 computer interface logic
Silicon oxide-silicon interface states at 77 degrees K
Hardware, software, and service interfaces between capsule bus, entry science package, and Voyager spacecraft
Hardware, software, and service interfaces between capsule bus, entry science package, surface laboratory, and Voyager spacecraft
Fluid interface instability suppression via feedback, noting stability criteria and parameters
Liquid-vapor interface in weightless environment noting dynamic behavior, configuration parameters and dependence on model size
Shear modulus effect on stress distribution of planar array of screw dislocations near bimetallic welded half-planes interface
Strength and durability in friction tests of soft, vacuum deposited, thin-metal gold film lubricants, noting dependence on film-substrate interface
Ballistic-electron-emission microscopy (BEEM) and spectroscopy have been used to investigate the properties of Au/GaN interfaces.
Measurements of the specific entropy argument of solar wind protons, T/n superscript y-1, reveal that nearly every occurrence of a high-speed stream seen at Ulysses in 1992-3 is characterized by an abrupt interface at its trailing edge.
This paper will describe the ways in which the Cassini Remote Terminal Interface Units were upgraded and enhanced to support flight operations during the Cassini tour of Saturn.
This viewgraph presentation reviews the architecture of the The CIA-AlA chip-set is a set of mixed-signal ASICs that provide a flexible high level interface between the spacecraft's command and data handling (C&DH) electronics and lower level functions in other spacecraft subsystems. Due to the open-systems architecture of the chip-set including an embedded micro-controller a variety of applications are possible. The chip-set was developed for the missions to the outer planets. The chips were developed to provide a single solution for both the switching and regulation of a spacecraft power bus. The Open-Systems Architecture allows for other powerful applications.
The task for this project was to design, develop, test, and deploy a facial recognition system for the Kennedy Space Center Augmented/Virtual Reality Lab. This system will serve as a means of user authentication as part of the NUI of the lab. The overarching goal is to create a seamless user interface that will allow the user to initiate and interact with AR and VR experiences without ever needing to use a mouse or keyboard at any step in the process.
Presentation that summarizes the 3D robot user interfaces developed by the ARC Intelligent Robotics Group.
Virtual Diagnostics Interface (ViDI), originally introduced by Richard Schwartz in 2004 and described again by Alderfer, et. al., in 2007, is an interactive 3D software tool developed at NASA Langley Research Center to serve three main purposes: assist in pre-test planning, enhance post-test image analysis and visualization, and serve as a central location for data storage and distribution.1,2 ViDI is composed of custom-developed software and Autodesk® 3ds Max® as it incorporates Computer Aided Design (CAD) models with the results obtained from optical diagnostics.3 This software tool has proven useful in the field of optical diagnostics where pre-test planning of beam paths, optical elements, and test articles must be carried out to avoid interference, ensure spatial resolution is sufficient, and the camera Field of View (FoV) is adequate for the field of interest. Typically, practical considerations such as the distance a camera is from the region of interest, the angles at which the camera is oriented and issues such as the size of the camera and its sensor and size and focal length lens as well as the path of the laser need to be taken into account to predict a successful measurement. An example application of ViDI is shown in Fig.1 where an experiment to investigate flow separation over the wing of the High Lift Common Research Model (HL-CRM) is currently being planned in the National Transonic Facility (NTF) at NASA Langley Research Center.
This paper describes the development of a vision-only intelligent interface for dexterous robots capable of tracking operator motions, analyzing trajectory feasibility, and providing visual feedback to the operator.
Correction to second approximation calculation of geomagnetic field, solar wind interface
Apparatus for measuring temperature drop across bolted interface