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|Other titles||Damage mitigating control of space propulsion systems for high performance and extended life.|
|Statement||Asok Ray and Min-Kuang Wu.|
|Series||NASA contractor report -- 194470., NASA contractor report -- NASA CR-194470.|
|Contributions||Wu, Min-Kuang., United States. National Aeronautics and Space Administration.|
|The Physical Object|
Download Damage-mitigating control of space propulsion systems for high performance and extended life
DAMAGE-MITIGATING CONTROL OF SPACE PROPULSION SYSTEMS FOR HIGH PERFORMANCE AND EXTENDED LIFE Report Prepared for NASA Lewis Research Center under Grant#: NAG by The Pennsylvania State University University Park, PA ABSTRACT A major goal in the control of complex mechanical systems such as spacecraft.
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[Asok Ray; Min-Kuang Wu; United States. National Aeronautics and. Ray, A. and Wu, M-K., b, “Damage-Mitigating Control of Space Propulsion Systems for High Performance and Extended Life,” NASA CR, Lewis Research Center, March.
RayCited by: Buy Damage-mitigating control of space propulsion systems for high performance and extended life (SuDoc NAS ) by Asok Ray (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : Asok Ray.
Damage-Mitigating Control of Power Systems for Structural Durability and High Performance M.-K. Wu, M.-K. b, “Damage-Mitigating Control of Space Propulsion Systems for High Performance and Extended Life,” NASA Contractor Report Royden, H, L.,Real Analysis, 3rd ed., Macmillan Publishing Company, New by: 1.
The concept of damage-mitigating control is to minimize fatigue (as well as creep and corrosion) damage of critical components of mechanical structures while simultaneously maximizing the system dynamic performance.
Given a dynamic model of the plant (for example, the turbofan engine, and frame of advanced aircraft, or the reusable rocket engine for space propulsion) and the specifications for.
Damage-mitigating control of a reusable rocket engine for high performance and extended life (English Edition) eBook: National Aeronautics and Space Administration NASA: : Kindle-Shop.
Request PDF | Damage-mitigating control of hypersonic flight vehicle based on prescribed performance | The goal of damage-mitigating control is to enhance the service life of complex mechanical.
AbstractA real-time optimization control method is proposed to extend turbo-fan engine service life. This real-time optimization control is based on an on-board engine mode, which is devised by a MRR-LSSVR (multi-input multi-output recursive reduced least squares support vector regression method).
To solve the optimization problem, a FSQP (feasible sequential quadratic programming) Cited by: 2. The primary space-based X-ray telescope is the Chandra X-Ray Observatory launched in The Japanese space agency's Suzaku X-ray Observatory (Japan's fifth x.
Damage-mitigating control of a reusable rocket engine for high performance and extended life eBook: National Aeronautics and Space Administration NASA: : Kindle Store.
The goal of damage-mitigating control in reusable rocket engines is to achieve high performance without overstraining the mechanical structures; and the major benefit is an increase in structural. You may not be able to, but your best bet would be to contact the Paris Opera itself.
Most opera houses sell libretti for the operas they produce. You might also try to find the address for the. Dai, X. and Ray, A. (a) Damage-mitigating control of the space shuttle main engine: Part I — Life prediction of the main thrust chamber wall. ASME Winter Annual Meeting, Chicago, and a revised version to appear in Journal of Dynamic Systems, Measurement and Control, September Author: Asok Ray, Shashi Phoha.
Dai and A. Ray, "Damage-Mitigating Control of a Reusable Rocket Engine: Part I -- Life Prediction of the Main Thrust Chamber Wall," Journal of Dynamic Systems, Measurement and Control-Transactions of the ASME, Vol.No.
3, Septemberpp. Caplin, Asok Ray and S. Joshi,"Robust damage-mitigating control of aircraft for high performance and structural durability", IEEE Transactions. Integrated Vehicle Health Management “Automated detection, diagnosis, prognosis to enable mitigation of adverse events manifest/escalate during flight and affect in-flight performance of aircraft systems, propulsion, and/or structure.
Integrate IRAC-developed damage mitigating control with experimental laboratory platform in Metric (i). Damage-mitigating control of space propulsion systems for high performance and extended life.
NASA Technical Reports Server (NTRS) Ray, Asok; Wu, Min-Kuang; Dai, Xiaowen; Carpino, Marc; Lorenzo, Carl F. Calculations are presented showing that a substantial improvement in service life of a reusable rocket engine can be achieved by an insignificant reduction.
American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA LPRE consist in one of the most complex propulsion systems for many reasons. Very high thrust forces (F) can be generated (until the order of 10 M N), corresponding to power amounts of 3 − 4 G W .Extreme temperature (T) differences are observed between cryogenic tanks, which can be at 20 K for liquid hydrogen; and combustion chamber core, which can surpass the by: 2.
Updated measurements of charged particle fluxes during the transit from Earth to Mars as well as on site measurements by Curiosity of Martian surface radiation fluxes identified potential health hazards associated with radiation exposure for human space missions.
Designing mitigation strategies of radiation risks to astronauts is critical. We investigated radiation-induced endothelial cell Cited by: 3. The paper studies the control of a class of discrete event processes, i.e., processes that are discrete, asynchronous and possibly nondeterministic.
The controlled process is described as the generator of a formal language, while the controller, or supervisor, is constructed from a recognizer for a specified target language that incorporates the desired closed-loop system by: () An implementation method for the supervisory control of time-driven systems applied to high-voltage direct current transmission grids.
Control Engineering Pract () Synthesis of minimally restrictive optimal stability-enforcing supervisors for nondeterministic discrete event by: The concept Propulsion system performance represents the subject, aboutness, idea or notion of resources found in Houston Public Library.
The paper studies the control of a class of discrete event processes, i.e., processes that are discrete, asynchronous and possibly nondeterministic. The controlled process is descCited by: Damage Tolerance of Candidate Thermoset Composites for use on Single Stage to Orbit Vehicles Damage-Mitigating Control of a Reusable Rocket Engine for High Performance and Extended Life Dark Companions of Stars Dark Matter in the Universe IAU Symposium No Darkness at Night A Riddle of the Universe Darwin and Astronomy: The Infrared Space.
Probabilistic performance-based design for high performance control systems. NASA Astrophysics Data System (ADS) Micheli, Laura; Cao, Liang; Gong, Yongqiang; Cancelli, Alessandro. This banner text can have markup. web; books; video; audio; software; images; Toggle navigation.
The Derbyshire Guardian is your innovative and interactive publication covering the the areas where you live and love. If you have something to shout about, whether it be a business success story. However, for larger aircraft with high wing spans, aerodynamic coupling between flight dynamic and aeroelastic motion becomes more significant because wing vibration frequencies are lower and closer to those of the flight dynamic modes F.
Stroscher (B) C. Breitsamter M. Meyer D. Paulus H. Baier Technische Universität München. Pennsylvania State University宾夕法尼亚州立大学航空航天工程硕士课程介绍_高等教育_教育专区 人阅读|2次下载. Pennsylvania State University宾夕法尼亚州立大学航空航天工程硕士课程介绍_高等教育_教 Read: Reliability Organizations x Reliability Society, IEEE, P.O. BoxPiscataway, New Jersey, U.S.A.
x SOLE, the International Society of Logistics, Professional Place, SuiteHyattsville, Maryland, U.S.A. x American Society for Quality Control, West Wisconsin Avenue, Milwaukee, Wisconsin, U.S.A. x National Aeronautics and. Advanced Fuzzy Logic Technologies in Industrial Applications Design Approach We design the fuzzy, PID, and sliding mode controllers based on the nominal plant given in Equation ().
Each designed controller is then applied to all three transfer functions, and numerical simulations are performed to analyze the controller's robustness. The new Teana is developed as a global model with an annual sales target of overunits in more than countries, including Japan, U.S.
and China. It will be sold as Altima in the U.S. and some other countries. It measures 4, mm long, 1, mm wide and 1, mm high, with a 2, mm wheelbase. EM [email protected] CRLINE FIRE ENG JAN, P29 *INNOVMETRIC SOFTW,POL IMINSPECT COMP V *ROLLS ROYC PLC,COMPR BLAD REP OVE, P10 BARDELL R,J MATER PROCESS TECH, V, P26 BREMER C,3 INT C LAS ASS NET CHEN LC,ROBOT CIM-INT MANUF, V16, P DIX B,INT J AIRER ENG AERO, V76 GAO J.
Modeling and Control for a Blended Wing Body Aircraft5/5(3).