Conferences related to Space vehicles

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2020 22nd European Conference on Power Electronics and Applications (EPE'20 ECCE Europe)

Energy conversion and conditioning technologies, power electronics, adjustable speed drives and their applications, power electronics for smarter grid, energy efficiency,technologies for sustainable energy systems, converters and power supplies


2020 59th IEEE Conference on Decision and Control (CDC)

The CDC is the premier conference dedicated to the advancement of the theory and practice of systems and control. The CDC annually brings together an international community of researchers and practitioners in the field of automatic control to discuss new research results, perspectives on future developments, and innovative applications relevant to decision making, automatic control, and related areas.


2020 IEEE International Conference on Robotics and Automation (ICRA)

The International Conference on Robotics and Automation (ICRA) is the IEEE Robotics and Automation Society’s biggest conference and one of the leading international forums for robotics researchers to present their work.


2020 IEEE International Conference on Systems, Man, and Cybernetics (SMC)

The 2020 IEEE International Conference on Systems, Man, and Cybernetics (SMC 2020) will be held in Metro Toronto Convention Centre (MTCC), Toronto, Ontario, Canada. SMC 2020 is the flagship conference of the IEEE Systems, Man, and Cybernetics Society. It provides an international forum for researchers and practitioners to report most recent innovations and developments, summarize state-of-the-art, and exchange ideas and advances in all aspects of systems science and engineering, human machine systems, and cybernetics. Advances in these fields have increasing importance in the creation of intelligent environments involving technologies interacting with humans to provide an enriching experience and thereby improve quality of life. Papers related to the conference theme are solicited, including theories, methodologies, and emerging applications. Contributions to theory and practice, including but not limited to the following technical areas, are invited.


2020 IEEE/ACM 42nd International Conference on Software Engineering (ICSE)

ICSE is the premier forum for researchers to present and discuss the most recent innovations,trends, outcomes, experiences, and challenges in the field of software engineering. The scopeis broad and includes all original and unpublished results of empirical, conceptual, experimental,and theoretical software engineering research.


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Periodicals related to Space vehicles

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Aerospace and Electronic Systems Magazine, IEEE

The IEEE Aerospace and Electronic Systems Magazine publishes articles concerned with the various aspects of systems for space, air, ocean, or ground environments.


Antennas and Propagation, IEEE Transactions on

Experimental and theoretical advances in antennas including design and development, and in the propagation of electromagnetic waves including scattering, diffraction and interaction with continuous media; and applications pertinent to antennas and propagation, such as remote sensing, applied optics, and millimeter and submillimeter wave techniques.


Antennas and Wireless Propagation Letters, IEEE

IEEE Antennas and Wireless Propagation Letters (AWP Letters) will be devoted to the rapid electronic publication of short manuscripts in the technical areas of Antennas and Wireless Propagation.


Applied Superconductivity, IEEE Transactions on

Contains articles on the applications and other relevant technology. Electronic applications include analog and digital circuits employing thin films and active devices such as Josephson junctions. Power applications include magnet design as well asmotors, generators, and power transmission


Automatic Control, IEEE Transactions on

The theory, design and application of Control Systems. It shall encompass components, and the integration of these components, as are necessary for the construction of such systems. The word `systems' as used herein shall be interpreted to include physical, biological, organizational and other entities and combinations thereof, which can be represented through a mathematical symbolism. The Field of Interest: shall ...


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Most published Xplore authors for Space vehicles

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Xplore Articles related to Space vehicles

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Deployable Mesh Reflector Antennas for Space Applications: RF Characterizations

Space Antenna Handbook, None

None


Technology '90: the main event (Voyager 2 project)

IEEE Spectrum, 1990

Voyager 2's flyby past the planet Neptune in August 1989 is recounted, focusing on its engineering achievements. The failure of its prime receiver only seven months after launch was followed by the failure of a tracking-loop capacitor in its backup receiver. Through clever engineering, that outage proved no more than an inconvenience. Its cameras were meant to work only in ...


Microelectronics or Plentary spacecraft

1991 IEEE International Solid-State Circuits Conference. Digest of Technical Papers, 1991

None


Space Environment and Materials

Space Antenna Handbook, None

None


Analysis of photoelectron effect on the antenna impedance via particle-in-cell simulation

Radio Science, 2008

We present photoelectron effects on the impedance of electric field antennas used for plasma wave investigations. To illustrate the photoelectron effects, we applied electromagnetic Particle-In-Cell simulation to the self-consistent antenna impedance analysis. We confirmed the formation of a dense photoelectron region around the sunlit surfaces of the antenna and the spacecraft. The dense photoelectrons enhance the real part, and decrease ...


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Educational Resources on Space vehicles

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IEEE-USA E-Books

  • Deployable Mesh Reflector Antennas for Space Applications: RF Characterizations

    None

  • Technology '90: the main event (Voyager 2 project)

    Voyager 2's flyby past the planet Neptune in August 1989 is recounted, focusing on its engineering achievements. The failure of its prime receiver only seven months after launch was followed by the failure of a tracking-loop capacitor in its backup receiver. Through clever engineering, that outage proved no more than an inconvenience. Its cameras were meant to work only in certain modes; en route Voyager's computers were reprogrammed with entirely new manoeuvers to stabilize an image and allow much longer exposures, so that resolution remained as good as in the images of its earlier, better-lit encounters.<<ETX>>

  • Microelectronics or Plentary spacecraft

    None

  • Space Environment and Materials

    None

  • Analysis of photoelectron effect on the antenna impedance via particle-in-cell simulation

    We present photoelectron effects on the impedance of electric field antennas used for plasma wave investigations. To illustrate the photoelectron effects, we applied electromagnetic Particle-In-Cell simulation to the self-consistent antenna impedance analysis. We confirmed the formation of a dense photoelectron region around the sunlit surfaces of the antenna and the spacecraft. The dense photoelectrons enhance the real part, and decrease the absolute value of the imaginary part, of antenna impedance at low frequencies. We also showed that the antenna conductance can be analytically calculated from simulation results of the electron current flowing into or out of the antenna. The antenna impedance in the photoelectron environment is represented by a parallel equivalent circuit consisting of a capacitance and a resistance, which is consistent with empirical knowledge. The results also imply that the impedance varies with the spin of the spacecraft, which causes the variation of the photoelectron density around the antenna.

  • Deep Space 1

    This chapter describes how the Deep Space 1 (DS1) spacecraft and the Deep Space Network (DSN) ground systems received and transmitted data. The signal to the spacecraft was at X‐band, and the signal to the ground was at X‐band or Ka‐band or both together. The chapter includes descriptions of the DSN systems used for carrier tracking, radiometric data, command transmission, and telemetry reception as DS1 used them through 2001. The telecom subsystem received and demodulated uplink commands, transmits science‐ and engineering‐telemetry data on either an X‐band or a Ka‐band downlink or both, and provided coherent two‐way Doppler and range‐measurement capabilities using the X‐band uplink, and the X‐ or Ka‐band downlink. The metric data assembly (MDA) at the tracking station processed DS1 Doppler data. The operational scenarios describe the major telecom‐subsystem operating modes in the context of supporting specific phases of the mission or major mission activities and modes.

  • The Microwave Reflectometers At Reentry Spacecraft And Plasma Sheath Diagnosing Results Analysis

    None

  • Aerospace and defense

    The challenge facing the European aerospace community after 1992, integrating members' individual capabilities into a decisively unified, noncontentious entity, is addressed. The two stellar examples of European cooperation in this area, the European Space Agency (ESA) and Arianespace SA, which builds and launches the Ariane rockets, are examined. ESA is a consortium of the national space research agencies of 13 countries and has overall responsibility for the development of Hermes, France's first manned space vehicle. Arianespace has 52 shareholder companies and research organizations in 11 countries; as the first company of its kind, it has captured more than half the world's commercial spacecraft launch-service business. The aerospace industry's biggest question, namely, what will happen in the defense sector, is discussed, focusing on the restructuring resulting from rising arms costs and changing political realities.<<ETX>>

  • Estimation of the solar flare neutron worst-case fluxes and fluences for missions traveling close to the Sun

    A method to estimate the total fluence of solar flare neutrons at a spacecraft traveling in the innermost part of the heliosphere (at heliocentric radial distances of <1 AU) is presented. The results of the neutron production and emissivity codes of Hua and Lingenfelter (1987a, 1987b) scaled to one of the largest solar neutron events ever observed at the Earth are used to derive a conservative estimate of the energy spectrum of neutrons emitted from the Sun after a large solar flare. By taking into account the survival probability of a neutron to reach a certain heliocentric distance, we evaluate the observed time-integrated spectrum of solar neutrons as a function of the heliocentric distance of the observer. By considering (1) a working relationship between the soft X-ray class of a flare and the flare's production of solar neutrons, and (2) the number and size of soft X-ray flares that may occur during a mission traveling close to the Sun, we compute an upper limit for the total fluence of solar neutrons at energies >1 MeV, >10 MeV, >100 MeV and >1000 MeV to which such a mission may be exposed. We apply this method to the Solar Probe Plus mission. Although our method gives a conservative estimate of neutron fluxes, the predicted mission-integrated fluence of solar neutrons at Solar Probe Plus is orders of magnitude below that of solar energetic protons.

  • The Deep Space Network

    This chapter describes the deep space network (DSN) as it is today. It includes brief descriptions and functional block diagrams of DSN systems at the Deep Space Communications Complexes that provide carrier tracking, radiometric data (Doppler and ranging) collection, command uplinking, and telemetry reception and decoding for deep space missions, those defined at lunar distances or greater. Delta‐differential one‐way ranging (delta‐DOR) is a very long baseline interferometric (VLBI) radio‐tracking technique using two deep‐space stations located at different complexes for a single measurement. In general, telemetry service support requires one antenna, at least one receiver, and telemetry processing equipment for each spacecraft. The telemetry system performs three main functions: data acquisition, data conditioning and transmission to projects, and telemetry‐system validation. The chapter summarizes the major uplink and downlink characteristics of the stations when operating in the DSN frequency bands.



Standards related to Space vehicles

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