Academic literature on the topic 'Aeronautics and Space Engineering Board'
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Journal articles on the topic "Aeronautics and Space Engineering Board"
Lindner, H. Greig. "Human Factors Support of Nasa's Safety Directorate on the Space Station Processing Facility (SSPF) Kennedy Space Center, FL." Proceedings of the Human Factors Society Annual Meeting 36, no. 13 (October 1992): 945–49. http://dx.doi.org/10.1177/154193129203601305.
Full textSztejnberg, Manuel, Shanjie Xiao, Nader Satvat, Felisa Limón, John Hopkins, and Tatjana Jevremovic. "Radiation shielding aspects for long manned mission to space: Criteria, survey study, and preliminary model." Nuclear Technology and Radiation Protection 21, no. 2 (2006): 47–66. http://dx.doi.org/10.2298/ntrp0602047s.
Full textKim, Yeanjae, Jieun Baek, and Yosoon Choi. "Smart Helmet-Based Personnel Proximity Warning System for Improving Underground Mine Safety." Applied Sciences 11, no. 10 (May 11, 2021): 4342. http://dx.doi.org/10.3390/app11104342.
Full textHirakata, Maki, Hajime Okamoto, Yuichiro Hagihara, Tadahiro Hayasaka, and Riko Oki. "Comparison of Global and Seasonal Characteristics of Cloud Phase and Horizontal Ice Plates Derived from CALIPSO with MODIS and ECMWF." Journal of Atmospheric and Oceanic Technology 31, no. 10 (October 1, 2014): 2114–30. http://dx.doi.org/10.1175/jtech-d-13-00245.1.
Full textFusaro, Roberta, Nicole Viola, Marco Fioriti, Davide Ferretto, and Sara Cresto Aleina. "Preliminary design of a cabin escape system for a suborbital vehicle aimed at parabolic flights." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 231, no. 12 (August 2, 2017): 2179–91. http://dx.doi.org/10.1177/0954410017723671.
Full textSalvi Sakamoto, João Marcos, and Gefeson Mendes Pacheco. "Laser ultrasonics in Brazil for aeronautics and space engineering." Physics Procedia 3, no. 1 (January 2010): 1081–85. http://dx.doi.org/10.1016/j.phpro.2010.01.140.
Full textRycroft, M. J. "Concise encyclopedia of aeronautics & space systems,." Journal of Atmospheric and Terrestrial Physics 57, no. 2 (February 1995): 213. http://dx.doi.org/10.1016/0021-9169(95)90003-9.
Full textJackson, Karen E., Yvonne T. Fuchs, and Sotiris Kellas. "Overview of the National Aeronautics and Space Administration Subsonic Rotary Wing Aeronautics Research Program in Rotorcraft Crashworthiness." Journal of Aerospace Engineering 22, no. 3 (July 2009): 229–39. http://dx.doi.org/10.1061/(asce)0893-1321(2009)22:3(229).
Full textSimanjuntak, Erni Br, and Gede Harja Wasistha. "VALUATION OF AERONAUTICS AND SPACE TECHNOLOGY AT LAPAN." AFEBI Economic and Finance Review 4, no. 01 (September 12, 2019): 1. http://dx.doi.org/10.47312/aefr.v4i01.212.
Full textBradshaw, T. W., and A. H. Orlowska. "Mechanical Cooling Systems for use in Space." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 207, no. 1 (January 1993): 21–25. http://dx.doi.org/10.1243/pime_proc_1993_207_242_02.
Full textDissertations / Theses on the topic "Aeronautics and Space Engineering Board"
Lohmeyer, Whitney Quinne. "Space radiation environment impacts on high power amplifiers and solar cells on-board geostationary communications satellites." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/98682.
Full textCataloged from PDF version of thesis.
Includes bibliographical references (pages 273-292).
Communications satellite operators maintain archives of component telemetry to monitor system function. Operators generally do not typically use the telemetry data for scientific analysis of the space radiation environment effects on component anomalies or performance. We partnered with four geostationary (GEO) operators, acquired >1 million hours of telemetry, and combined these data with space weather observations to investigate relationships between space weather and hardware performance. We focused on the effects of space weather on two component types: solar cells and high power amplifiers. For solar cells, by augmenting >20 years of GEO telemetry with separate GEO space weather measurements, we calculated both on-orbit degradation of Si and GaAs solar cells in an annual average sense, and also quantified the degradation of cells during severe solar proton events (SPEs) of 10 MeV protons > 10,000 pfu. A functional relationship between the amount of degradation and proton fluence is also considered. We used the calculated degradation to evaluate several combinations of space weather environment models with solar cell degradation models and found that predicted performance is within 1% of the observed degradation. These models had not previously been validated using multiple on-orbit GEO datasets. We did not find a model pairing that consistently outperformed the others over all of the datasets. For high power amplifiers, through the use of statistical analysis, simulations, and electron beam experiments we conducted a root-cause analysis of solid state power amplifier (SSPA) anomalies on-board eight GEO satellites. From the statistical analysis, we identified that the occurrence of anomalies was not random with respect to the space weather environment, but that there appeared to be a relationship to high-energy electron fluence for periods of time between 10 - 21 days before the anomalies. From the simulations and electron beam lab tests, we demonstrated that internal charging occurs in the amplifier chain, potentially identifying a cause for the observed anomalies. We substantiated an approach toward understanding space weather effects on space components by obtaining and using long-duration archives of standard commercial telemetry for scientific analysis. The analysis of large telemetry data sets of similar components over long periods of time improves our ability to assess the role of different types of space weather events in causing anomalies and helps to validate models. The findings in this work that relate deep dielectric charging to component anomalies and solar proton events to solar cell degradation make use of only a small fraction of the potentially available commercial geostationary satellite telemetry. Expansion of this work would provide additional insights on the role of space weather to the science community and to the satellite design and operator community.
by Whitney Quinne Lohmeyer.
Ph. D.
Bilton, Amy M. (Amy Marlou). "Fusion of remote vision and on-board acceleration data for the vibration estimation of large space structures." Thesis, Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/35580.
Full textIncludes bibliographical references (leaves 81-84).
Future space structures such as solar power stations and telescopes are expected to be very large. These structures will require on-orbit construction. Due to the risks and costs of human extravehicular work, teams of robots will be essential for the on-orbit assembly of the large space structures. There are a number of technical challenges presented by such robotic construction. The structures will need to be made of lightweight materials and will be very flexible. Autonomous robots will require information about the vibrations of the flexible structures and their dynamic parameters in order to perform the construction efficiently. Often models of the structures are imperfect, therefore the magnitude of the vibrations of the structure must be estimated on-orbit. This thesis presents a method for estimating the shape and dynamic parameters of a vibrating large space structure. This technique is a cooperative sensing approach using remote free-flying robot observers equipped with vision sensors and structure-mounted accelerometers. This approach exploits the complementary nature of the two types of sensors.
(cont.) Vision sensors are able to measure structure deflections at a high spatial frequency but are bandwidth limited. Accelerometers are able to make measurements at high temporal frequency, but are sparsely located on the structure. The fused estimation occurs in three steps. First, the vision data is condensed in a modal decomposition that results in coarse estimates of modal coefficients. In the second step, the coarse estimates of the modal coefficients obtained from vision data are fused with the accelerometer measurements in a multi-rate nonlinear Kalman filter, resulting in a refined estimate of the modal coefficients and dynamic properties of the structure. In the final step, the estimated modal coefficients are combined with the mode shapes to provide a shape estimate of the entire structure. Simulation and experimental results demonstrate that the performance of this fused estimation approach is superior to the performance achieved when using only a single type of sensor.
by Amy M. Bilton.
S.M.
Meyen, Forrest Edward. "Engineering a robotic exoskeleton for space suit simulation." Thesis, Massachusetts Institute of Technology, 2013. http://hdl.handle.net/1721.1/85810.
Full textCataloged from PDF version of thesis.
Includes bibliographical references (pages 177-181).
Novel methods for assessing space suit designs and human performance capabilities are needed as NASA prepares for manned missions beyond low Earth orbit. Current human performance tests and training are conducted in space suits that are heavy and expensive, characteristics that constrain possible testing environments and reduce suit availability to researchers. Space suit mock-ups used in planetary exploration simulations are light and relatively inexpensive but do not accurately simulate the joint stiffness inherent to space suits, a key factor impacting extravehicular activity performance. The MIT Man-Vehicle Laboratory and Aurora Flight Sciences designed and built an actively controlled exoskeleton for space suit simulation called the Extravehicular Activity Space Suit Simulator (EVA S3), which can be programmed to simulate the joint torques recorded from various space suits. The goal of this research is to create a simulator that is lighter and cheaper than a traditional space suit so that it can be used in a variety of testing and training environments. The EVA S3 employs pneumatic actuators to vary joint stiffness and a pre-programmed controller to allow the experimenter to apply torque profiles to mimic various space suit designs in the field. The focus of this thesis is the design, construction, integration, and testing of the hip joint and backpack for the EVA S3. The final designs of the other joints are also described. Results from robotic testing to validate the mechanical design and control system are discussed along with the planned improvements for the next iteration of the EVA S3. The fianl EVA S3 consists of a metal and composite exoskeleton frame with pneumatic actuators that control the resistance of motion in the ankle, knee, and hip joints, and an upper body brace that resists shoulder and elbow motions with passive spring elements. The EVA S3 is lighter (26 kg excluding the tethered components) and less expensive (under $600,000 including research, design, and personnel) than a modem space suit. Design adjustments and control system improvements are still needed to achieve a desired space suit torque simulation fidelity within 10% root-mean-square error.
by Forrest Edward Meyen.
S.M.
Newman, Dava Jean. "Human mental workload & performance in space : engineering development and policy aspects." Thesis, Massachusetts Institute of Technology, 1989. http://hdl.handle.net/1721.1/41233.
Full textTilly, John G. (John Gilbert) 1978. "Making handheld divices smaller : a boost converter that uses minimum board space." Thesis, Massachusetts Institute of Technology, 2001. http://hdl.handle.net/1721.1/86729.
Full textIncludes bibliographical references (leaves 68-69).
by John G. Tilly.
M.Eng.
Holschuh, Bradley Thomas. "Space exploration challenges : characterization and enhancement of space suit mobility and planetary protection policy analysis." Thesis, Massachusetts Institute of Technology, 2010. http://hdl.handle.net/1721.1/62036.
Full textThis electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
Cataloged from student-submitted PDF version of thesis.
Includes bibliographical references (p. 189-193).
This thesis addresses two challenges associated with advanced space and planetary exploration: characterizing and improving the mobility of current and future gas pressurized space suits; and developing effective domestic Planetary Protection policies for the emerging private space industry. Gas-pressurized space suits are known to be highly resistive to astronaut movement. As NASA seeks to return to planetary exploration, there is a critical need to improve full body space suit mobility for planetary exploration. Volume effects (the torque required to displace gas due to internal volume change during movement) and structural effects (the additional torque required to bend the suit materials in their pressurized state) are cited as the primary contributors to suit rigidity. Constant volume soft joints have become the design goal of space suit engineers, and simple joints like the elbow are believed to have nearly achieved such performance. However, more complex joints like the shoulder and waist have not yet achieved comparable optimization. As a result, it is hypothesized that joints like the shoulder and waist introduce a third, and not well studied, contributor to space suit rigidity: pressure effects (the additional work required to compress gas in the closed operating volume of the suit during movement). This thesis quantifies the individual contributors to space suit rigidity through modeling and experimentation. An Extravehicular Mobility Unit (EMU) space suit arm was mounted in a -30kPa hypobaric chamber, and both volume and torque measurements were taken versus elbow angle. The arm was tested with both open and closed operating volumes to determine the contribution of pressure effects to total elbow rigidity. These tests were then repeated using a full EMU volume to determine the actual impact of elbow pressure effects on rigidity when connected to the full suit. In both cases, structural and volume effects were found to be primary contributors to elbow joint rigidity, with structural effects dominating at low flexion angles and volume effects dominating at high flexion angles; pressure effects were detected in the tests that used only the volume of the arm, but were found to be a secondary contributor to total rigidity (on average < 5%). These pressure effects were not detected in the tests that used the volume representative of a full EMU. Unexpected structural effects behavior was also measured at high (> 75°) flexion angles, suggesting that the underlying mechanisms of these effects are not yet fully understood, and that current models predicting structural effects behavior do not fully represent the actual mechanisms at work. The detection of pressure effects in the well-optimized elbow joint, even if only in a limited volume, suggests that these effects may prove significant for sub-optimized, larger, multi-axis space suit joints. A novel, fast-acting pressure control system, developed in response to these findings, was found to be capable of mitigating pressure spikes due to volume change (and thus, pressure effects). Implementation of a similar system in future space suit designs could lead to improvements in overall suit mobility. A second study, which focused on the implications of the development of the US private space industry on domestic Planetary Protection policy, is also presented. As signatories of the 1967 Treaty on Principles Governing the Activities of States in the Exploration and Use of Outer Space (commonly known as the Outer Space Treaty), the United States is responsible for implementing Planetary Protection procedures designed to prevent biological contamination of the Solar System, as well as contamination of the Earth by any samples returned from extra-terrestrial bodies. NASA has established policies and procedures to comply with this treaty, and has successfully policed itself independently and autonomously since the signing of the treaty. However, for the first time in the history of the American space program, private entities outside of NASA have developed the capability and interest to send objects into space and beyond Earth orbit, and no current protocol exists to guarantee these profit-minded entities comply with US Planetary Protection obligations (a costly and time-consuming process). This thesis presents a review of US Planetary Protection obligations, including NASA's procedures and infrastructure related to Planetary Protection, and based on these current protocols provides policy architecture recommendations for the emerging commercial spaceflight industry. It was determined that the most effective policy architecture for ensuring public and private compliance with Planetary Protection places NASA in control of all domestic Planetary Protection matters, and in this role NASA is charged with overseeing, supporting, and regulating the private spaceflight industry. The underlying analysis and architecture tradeoffs that led to this recommendation are presented and discussed.
by Bradley Thomas Holschuh.
S.M.in Technology and Policy
S.M.
Reynerson, Charles Martin. "Design considerations for remotely operated welding in space : task definition and visual weld monitoring experiment." Thesis, Massachusetts Institute of Technology, 1993. http://hdl.handle.net/1721.1/47326.
Full textIncludes bibliographical references (leaves 237-245).
by Charles Martin Reynerson.
E.A.A.
Nav.E.
Upadhyay, Indrima. "ANALYSIS OF Q- LEARNING BASED GAME PLAYING AGENTS FOR ABSTRACT BOARD GAMES WITH INCREASING STATE-SPACE COMPLEXITY." Miami University / OhioLINK, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=miami1627681408588176.
Full textViggh, Herbert E. M. "Artificial intelligence applications in teleoperated robotic assembly of the EASE space structure." Thesis, Massachusetts Institute of Technology, 1988. http://hdl.handle.net/1721.1/39358.
Full textBibliography: leaf 197.
by Herbert E. M. Viggh.
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, and Dept. of Electrical Engineering and Computer Science, 1988.
Sutherland, Timothy A. (Timothy Alan). "Stakeholder value network analysis for space-based earth observations." Thesis, Massachusetts Institute of Technology, 2009. http://hdl.handle.net/1721.1/63181.
Full textThis electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
Cataloged from student-submitted PDF version of thesis.
Includes bibliographical references (p. 237-238).
The Earth Science and Applications decadal survey released by the National Research Council in 2007 presents both an ambitious engineering challenge and a challenge for the entire Earth science community to come together to reach a consensus on priorities that cross conventional disciplinary boundaries. The vision established by the decadal survey requires a paradigm shift for Earth system science: Societal benefits must be considered equally with purely scientific benefits to guide the development of the future NASA and NOAA Earth Observations Program. The decadal survey focused heavily on the needs and objectives of the Earth science community, while providing much less thorough treatment of the other relevant stakeholders. To address this, I conducted a stakeholder value network analysis for the Earth Observations Program that includes the development of a comprehensive qualitative and quantitative stakeholder model. The qualitative model includes a rigorous articulation of the needs and objectives of 13 major stakeholders; the development of a three-level stakeholder map including a baseline map, higher-level map, and lower-level map; and a complete stakeholder value network model with 190 individual value flows that capture the interactions between all the stakeholders. The quantitative model includes a method for assigning numeric scores to each value flow; the calculation of 1880 unique and valid "value loops" within the stakeholder value network; and an analysis of the value loops that yields useful insights about the Earth Observations Program. The value loop analysis reveals the most important stakeholders, value flows, and value loops within the stakeholder value network; as well as the most important outputs from and inputs to NASA and NOAA. The analysis also reveals the relative important of each of the six science categories representing the six science-themed panels of the decadal survey. The results from the stakeholder value network analysis provide insights regarding the value produced by the Earth Observations Program, as well as the value-added roles of each stakeholder within the network. The most important value loops and Program outputs are used to derive a set of high-level program goals, including goals that suggest what NASA and NOAA should do, as well as how they should conduct business. Finally, the insights and results from the analysis provide the foundation for a set of recommendations for the Earth Observations Program, which complement the recommendations put forth in the decadal survey.
by Timothy A. Sutherland.
S.M.in Technology and Policy
S.M.
Books on the topic "Aeronautics and Space Engineering Board"
Pelt, Michel Van. Space tethers and space elevators. New York: Copernicus Books, 2009.
Find full textEngineering the space age: A rocket scientist remembers. Maxwell Air Force Base, Ala: Air University Press, 2008.
Find full textShishko, Robert. NASA systems engineering handbook. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Find full textShishko, Robert. NASA systems engineering handbook. [Washington, D.C.?]: National Aeronautics and Space Administration, 1995.
Find full textShishko, Robert. NASA systems engineering handbook. [Washington, D.C.?]: National Aeronautics and Space Administration, 1995.
Find full textPearson, Lillian. Design of a vibration isolation system for a cycle ergometer to be used on board the space shuttle. Austin, Tex: Mechanical Engineering Design Projects Program, University of Texas at Austin, 1991.
Find full textPearson, Lillian. Design of a vibration isolation system for a cycle ergometer to be used on board the space shuttle. Austin, Tex: Mechanical Engineering Design Projects Program, University of Texas at Austin, 1991.
Find full textThe space shuttle: Celebrating thirty years of NASA's first space plane. Minneapolis: MBI Pub. Co. and Zenith Press, 2011.
Find full textUnited States. Columbia Accident Investigation Board. Columbia Accident Investigation Board: Report. Burlington, Ont: Apogee Books, 2003.
Find full textBook chapters on the topic "Aeronautics and Space Engineering Board"
Nuñez, Miguel David Ruiz-Cabello, Sergio Fernández Romero, Marc Pous, Enrique Pascual Gil, Luis M. Diaz Angulo, David Poyatos Martínez, Mireya Fernández Chimeno, et al. "Numerical Assessment in Aeronautics for Electromagnetic Environmental Effects." In Electromagnetic Compatibility for Space Systems Design, 153–210. IGI Global, 2018. http://dx.doi.org/10.4018/978-1-5225-5415-8.ch005.
Full textFehring, Thomas H., and Terry S. Reynolds. "Aviation and Aerospace." In Chronicles of Mechanical Engineering in the United States, 251–309. ASME, 2021. http://dx.doi.org/10.1115/1.356056_ch7.
Full textNebdi, Hamid. "Space Weather and Link to Climate Change." In Advances in Environmental Engineering and Green Technologies, 1–20. IGI Global, 2019. http://dx.doi.org/10.4018/978-1-5225-7775-1.ch001.
Full textPapastamatis, Panagiotis K., Eleni P. Nicolopoulou, and Ioannis F. Gonos. "Electromagnetic Compatibility Testing for Space Systems." In Recent Trends on Electromagnetic Environmental Effects for Aeronautics and Space Applications, 97–126. IGI Global, 2021. http://dx.doi.org/10.4018/978-1-7998-4879-0.ch004.
Full textPiecka, Debra C. Burkey, Laurie Ruberg, Christopher Ruckman, and Dynae Fullwood. "NASATalk as a Discovery Learning Space." In Constructing Self-Discovery Learning Spaces Online, 49–71. IGI Global, 2012. http://dx.doi.org/10.4018/978-1-61350-320-1.ch004.
Full textFain, Stacie L. "2025." In Civil and Environmental Engineering, 1663–70. IGI Global, 2016. http://dx.doi.org/10.4018/978-1-4666-9619-8.ch076.
Full textHerzig, Sebastian J. I., and Christiaan J. J. Paredis. "Probabilistic Reasoning and Inconsistency Identification in Graph-based Models." In Advances in Computers and Information in Engineering Research, Volume 2, 533–63. ASME, 2021. http://dx.doi.org/10.1115/1.862025_ch17.
Full textHendrickson, Susan M., and Margo E. Young. "Electronic Records Management at a Federally Funded Research and Development Center." In Cases on Electronic Records and Resource Management Implementation in Diverse Environments, 334–50. IGI Global, 2014. http://dx.doi.org/10.4018/978-1-4666-4466-3.ch020.
Full textSánchez, Javier Ruiz, and María José Martínez Sánchez. "Sensitive Bodies in the Cityscape." In Advances in Civil and Industrial Engineering, 260–76. IGI Global, 2018. http://dx.doi.org/10.4018/978-1-5225-3637-6.ch011.
Full textBaggag, Abdelkader, Harold Atkins, and David Keyes. "Parallel Implementation of the Discontinuous Galerkin Method * *This research was supported by the National Aeronautics and Space Administration under NASA contract No. NAS1-97046 while Baggag and Keyes were in residence at the Institute for Computer Applications in Science and Engineering (ICASE), NASA Langley Research Center, Hampton, VA 23681-2199." In Parallel Computational Fluid Dynamics 1999, 115–22. Elsevier, 2000. http://dx.doi.org/10.1016/b978-044482851-4.50015-3.
Full textConference papers on the topic "Aeronautics and Space Engineering Board"
McCurdy, Kerri, Arturo Vasquez, and Karla Bradley. "Development of PEMFC Systems for Space Power Applications." In ASME 2003 1st International Conference on Fuel Cell Science, Engineering and Technology. ASMEDC, 2003. http://dx.doi.org/10.1115/fuelcell2003-1726.
Full textBenson, James W. "Private Space Exploration Is Here: Are You On-Board?" In Sixth ASCE Specialty Conference and Exposition on Engineering, Construction, and Operations in Space. Reston, VA: American Society of Civil Engineers, 1998. http://dx.doi.org/10.1061/40339(206)4.
Full textBos, Victor, Timo Vepsalainen, Yuliya Prokhorova, and Timo Latvala. "Time and Space Partitioning Using On-Board Software Reference Architecture." In 2016 IEEE International Symposium on Software Reliability Engineering Workshops (ISSREW). IEEE, 2016. http://dx.doi.org/10.1109/issrew.2016.49.
Full textCoffelt, Everett L., and Mark A. Martella. "Optical filters on board the Space Telescope Imaging Spectrograph (STIS)." In SPIE's 1996 International Symposium on Optical Science, Engineering, and Instrumentation, edited by Robert E. Fischer and Warren J. Smith. SPIE, 1996. http://dx.doi.org/10.1117/12.256239.
Full textUlin, Sergey E., K. F. Vlasik, A. M. Galper, V. M. Grachev, Valery V. Dmitrenko, S. N. Zherebtsov, V. M. Kamaev, et al. "Gamma spectrometer XENON for space gamma burst study on board ISS." In SPIE's International Symposium on Optical Science, Engineering, and Instrumentation, edited by F. P. Doty and Richard B. Hoover. SPIE, 1998. http://dx.doi.org/10.1117/12.312880.
Full textBorisova, Margarita, and Almaz Kamalov. "Features of Space Charge Relaxation in a Polyimide Printed Circuit Board." In 2018 IEEE International Conference on Electrical Engineering and Photonics (EExPolytech). IEEE, 2018. http://dx.doi.org/10.1109/eexpolytech.2018.8564364.
Full textLyver, John W., Peter G. Prassinos, and Chinh T. Bui. "Designing in Safety Through Early Safety Requirements Management." In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-63500.
Full textBagnasco, Giorgio, Manfred Kolm, Pierre Ferruit, Karl Honnen, Jess Koehler, Robert Lemke, Marc Maschmann, et al. "Overview of the near-infrared spectrograph (NIRSpec) instrument on-board the James Webb Space Telescope (JWST)." In Optical Engineering + Applications, edited by James B. Heaney and Lawrence G. Burriesci. SPIE, 2007. http://dx.doi.org/10.1117/12.735602.
Full textChaiyot, Rungwicha, and Vijit Kinnares. "Continuous and discontinuous space vector pulsewidth modulator using a TMS320C2000 F28335 Board." In 2016 13th International Conference on Electrical Engineering/Electronics, Computer, Telecommunications and Information Technology (ECTI-CON). IEEE, 2016. http://dx.doi.org/10.1109/ecticon.2016.7561444.
Full textAli, Hadi, and Robin Adams. "Configuration Control Board Activities during the Development of the Apollo Lunar Module: Insight into the \Art" of System Engineering." In AIAA SPACE 2012 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-5196.
Full text