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NASA Technical Reports Server (NTRS) 19980201707: Use of microgravity sensors for quantification of
In the modeling of spacecraft dynamics it is important to accurately characterize the environment in which the vehicle operates, including the environments induced by the vehicle itself. On the Space ...
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Sensitivity Analysis: Matrix Methods in Demography and Ecology
...
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Problems in Classical Electromagnetism
157 Exercises with Solutions...
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Monitoring Direct Effects of Delta, Atlas, and Titan Launches from Cape Canaveral Air Station
Launches of Delta, Atlas, and Titan rockets from Cape Canaveral Air Station (CCAS) have potential environmental effects that could arise from direct impacts of the launch exhaust (e.g., blast, heat), ...
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NASA Technical Reports Server (NTRS) 19910012770: Multiaxis thrust vectoring using axisymmetric nozz
A ground-based investigation was conducted on an operational system of multiaxis thrust vectoring using postexit vanes around an axisymmetric nozzle. This thrust vectoring system will be tested on the...
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Enhanced Living Environments
Algorithms, Architectures, Platforms, and Systems...
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NASA Technical Reports Server (NTRS) 19780016328: Orbiter/payload proximity operations SES Postsim r
Various approach and stationkeeping simulations (proximity operations) were conducted in the Shuttle engineering simulator (SES). This simulator is the first to dynamically include the Orbiter reactio...
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Algorithmic Graph Theory and Sage
...
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NASA Technical Reports Server (NTRS) 19930012247: Operator-assisted planning and execution of proxim
Future multi-vehicle operations will involve multiple scenarios that will require a planning tool for the rapid, interactive creation of fuel-efficient trajectories. The planning process must deal wit...
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Linear Selection Indices in Modern Plant Breeding
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Programming Computer Vision with Python
Tools and algorithms for analyzing images...
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Anisotropy Across Fields and Scales
...
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NASA Technical Reports Server (NTRS) 20090022233: Particle Ejection and Levitation Technology (PELT)
Each of the six Apollo landers touched down at unique sites on the lunar surface. Aside from the Apollo 12 landing site located 180 meters from the Surveyor III lander, plume impingement effects on gr...
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Solving PDEs in Python
The FEniCS Tutorial I...
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NASA Technical Reports Server (NTRS) 19870004995: An analytical and experimental investigation of re
As a part of the electrothermal propulsion plume research program at the NASA Lewis Research Center, efforts have been initiated to analytically and experimentally investigate the plumes of resistojet...
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Foundations of Machine Learning
...
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Ionospheric Multi-Spacecraft Analysis Tools
Approaches for Deriving Ionospheric Parameters...
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Software for Exascale Computing - SPPEXA 2016-2019
...
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Finite Difference Computing with PDEs
A Modern Software Approach...
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Russia's Turn to the East
Domestic Policymaking and Regional Cooperation...
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Spatial Thinking in Planning Practice
An Introduction to GIS...
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Signal Computing
Digital Signals in the Software Domain...
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Variant Construction from Theoretical Foundation to Applications
...
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DTIC ADA505275: Methodology and Historical Perspective of a Hall Thruster Efficiency Analysis
A Hall thruster performance architecture was developed based on separation of the total thrust directed along thruster centerline into mass weighted and momentum-weighted terms. With this formulation,...
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Interface Oral Health Science 2016
Innovative Research on Biosis–Abiosis Intelligent Interface...
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NASA Technical Reports Server (NTRS) 20020062709: Translation Optics for 30 cm Ion Engine Thrust Vec
Data were obtained from a 30 cm xenon ion thruster in which the accelerator grid was translated in the radial plane. The thruster was operated at three different throttle power levels, and the acceler...
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Data Parallel C++
Mastering DPC++ for Programming of Heterogeneous Systems using C++ and SYCL...
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NASA Technical Reports Server (NTRS) 19950004420: Interactive orbital proximity operations planning
This guide instructs users in the operation of a Proximity Operations Planning System. This system uses an interactive graphical method for planning fuel-efficient rendezvous trajectories in the multi...
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Programming for Computations - Python
A Gentle Introduction to Numerical Simulations with Python 3.6...
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Clinical Text Mining
Secondary Use of Electronic Patient Records...
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Pro TBB
C++ Parallel Programming with Threading Building Blocks...
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Analysis for Computer Scientists
Foundations, Methods, and Algorithms...
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Bayesian Methods in the Search for MH370
...
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Intelligent Human Computer Interaction
9th International Conference, IHCI 2017, Evry, France, December 11-13, 2017, Proceedings...
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NASA Technical Reports Server (NTRS) 20120002932: Exhaust Nozzle Plume Effects on Sonic Boom Test Re
Reducing or eliminating the operational restrictions of supersonic aircraft over populated areas has led to extensive research at NASA. Restrictions were due to the disturbance of the sonic boom, caus...
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DTIC ADA489529: Standardization of Hall Thruster Efficiency Analysis: Methodology and Historical Per
The rocket power efficiency equation was analytically decomposed to explicitly account for the effects of energy conversion losses, plume divergence, and the velocity distribution function of the prop...
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Foundations of Quantum Theory
From Classical Concepts to Operator Algebras...
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Fundamentals of Biomechanics
Equilibrium, Motion, and Deformation...
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Health of People, Health of Planet and Our Responsibility
Climate Change, Air Pollution and Health...
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Intel Xeon Phi Coprocessor Architecture and Tools
The Guide for Application Developers...
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Physical (A)Causality
Determinism, Randomness and Uncaused Events...
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Understanding Machine Learning
From Theory to Algorithms...
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Introduction to Data Science
Data Analysis and Prediction Algorithms with R...
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NASA Technical Reports Server (NTRS) 19960002903: NSTAR Ion Thruster Plume Impact Assessments
Tests were performed to establish 30-cm ion thruster plume impacts, including plume characterizations via near and farfield ion current measurements, contamination, and sputtering assessments. Current...
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International Symposium on Mathematics, Quantum Theory, and Cryptography
Proceedings of MQC 2019...
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Developing Graphics Frameworks with Python and OpenGL
...
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Representation Learning for Natural Language Processing
...
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NASA Technical Reports Server (NTRS) 19800002891: Specific spacecraft evaluation: Special report. [c
Charged and neutral particle transport from an 8 cm mercury ion thruster to the surfaces of the P 80-1 spacecraft and to the Teal Ruby sensor and the ECOM-501 sensor of that spacecraft were investigat...
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NASA Technical Reports Server (NTRS) 20000121256: Pulsed Plasma Thruster Plume Study: Symmetry and I
Twenty-four witness plates were positioned on perpendicular arrays near a breadboard Pulsed Plasma Thruster (PPT) to collect plume constituents for analysis. Over one million shots were fired during t...
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Spectral and High Order Methods for Partial Differential Equations ICOSAHOM 2018
Selected Papers from the ICOSAHOM Conference, London, UK, July 9-13, 2018...
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Digital Video Concepts, Methods, and Metrics
Quality, Compression, Performance, and Power Trade-off Analysis...
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Ambisonics
A Practical 3D Audio Theory for Recording, Studio Production, Sound Reinforcement, and Virtual Reality...
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Optimizing software in C++
An optimization guide for Windows, Linux and Mac platforms...
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Optimizing HPC Applications with Intel Cluster Tools
Hunting Petaflops...
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Language Technologies for the Challenges of the Digital Age
27th International Conference, GSCL 2017, Berlin, Germany, September 13-14, 2017, Proceedings...
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Annotated Algorithms in Python
With applications in Physics, Biology, and Finance...
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Fractional Graph Theory
A Rational Approach to the Theory of Graphs...
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NASA Technical Reports Server (NTRS) 20090014050: Sonic Boom Research at NASA Dryden: Objectives and
The principal objective of the Supersonics Project is to develop and validate multidisciplinary physics-based predictive design, analysis and optimization capabilities for supersonic vehicles. For air...
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NASA Technical Reports Server (NTRS) 20100039414: Use of ILTV Control Laws for LaNCETS Flight Resear
A report discusses the Lift and Nozzle Change Effects on Tail Shock (LaNCETS) test to investigate the effects of lift distribution and nozzle-area ratio changes on tail shock strength of an F-15 aircr...
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Error-Correction Coding and Decoding
Bounds, Codes, Decoders, Analysis and Applications...
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Biodiversity and Health in the Face of Climate Change
...
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Statistics with Julia
Fundamentals for Data Science, Machine Learning and Artificial Intelligence...
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Efficient Learning Machines
Theories, Concepts, and Applications for Engineers and System Designers...
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CIA Reading Room cia-rdp94b00280r000700190003-9: BRIEFINGS AND REPORTS
Sanitized Copy Approved for Release 2011/03/11: CIA-RDP94B0028OR000700190003-9 Next 1 Page(s) In Document Denied Iq Sanitized Copy Approved for Release 2011/03/11: CIA-RDP94B0028OR000700190003-9 TITAN...
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DTIC ADA507397: Moth-Inspired Chemical Plume Tracing on an Autonomous Underwater Vehicle
This paper presents a behavior-based adaptive mission planner (AMP) to trace a chemical plume to its source and reliably declare the source location. The proposed AMP is implemented on a REMUS autonom...
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NASA Technical Reports Server (NTRS) 19930007369: Volume 2: Explicit, multistage upwind schemes for
The objective of this study was to develop a high-resolution-explicit-multi-block numerical algorithm, suitable for efficient computation of the three-dimensional, time-dependent Euler and Navier-Stok...
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