Conferences related to Aeronautical And Space Sensor Systems

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2021 IEEE/MTT-S International Microwave Symposium - IMS 2021

The IEEE MTT-S International Microwave Symposium (IMS) is the premier conference covering basic technologies, to passives and actives components to system over a wide range of frequencies including VHF, UHF, RF, microwave, millimeter-wave, terahertz, and optical. The conference will encompass the latest in RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation, wireless systems, RFID and related topics.

  • 2006 IEEE/MTT-S International Microwave Symposium - MTT 2006

  • 2007 IEEE/MTT-S International Microwave Symposium - MTT 2007

  • 2008 IEEE/MTT-S International Microwave Symposium - MTT 2008

  • 2009 IEEE/MTT-S International Microwave Symposium - MTT 2009

    The IEEE International Microwave Symposium (IMS) is the world s foremost conference covering the UHF, RF, wireless, microwave, millimeter-wave, terahertz, and optical frequencies; encompassing everything from basic technologies to components to systems including the latest RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation and more. The IMS includes technical and interactive sessions, exhibits, student competitions, panels, workshops, tutorials, and networking events.

  • 2010 IEEE/MTT-S International Microwave Symposium - MTT 2010

    Reports of research and development at the state-of-the-art of the theory and techniques related to the technology and applications of devices, components, circuits, modules and systems in the RF, microwave, millimeter-wave, submillimeter-wave and Terahertz ranges of the electromagnetic spectrum.

  • 2011 IEEE/MTT-S International Microwave Symposium - MTT 2011

    The IEEE International Microwave Symposium (IMS) is the world s foremost conference covering the UHF, RF, wireless, microwave, millimeter-wave, terahertz, and optical frequencies; encompassing everything from basic technologies to components to systems including the latest RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation and more. The IMS includes technical and interactive sessions, exhibits, student competitions, panels, workshops, tutorials, and networking events.

  • 2012 IEEE/MTT-S International Microwave Symposium - MTT 2012

    The IEEE International Microwave Symposium (IMS) is the world s foremost conference covering the UHF, RF, wireless, microwave, millimeter-wave, terahertz, and optical frequencies; encompassing everything from basic technologies to components to systems including the latest RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation and more. The IMS includes technical and interactive sessions, exhibits, student competitions, panels, workshops, tutorials, and networking events.

  • 2013 IEEE/MTT-S International Microwave Symposium - MTT 2013

    The IEEE MTT-S International Microwave Symposium (IMS) is the premier conference covering basic technologies, to passives and actives components to system over a wide range of frequencies including VHF, UHF, RF, microwave, millimeter -wave, terahertz, and optical. The conference will encompass the latest in RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation, wireless systems, RFID and related topics.The IMS includes technical and interactive sessions, exhibits, student competitions, panels, workshops, tutorials, and networking events.

  • 2014 IEEE/MTT-S International Microwave Symposium - MTT 2014

    IMS2014 will cover developments in microwave technology from nano devices to system applications. Technical paper sessions, interactive forums, plenary and panel sessions, workshops, short courses, industrial exhibits, and a wide array of other technical activities will be offered.

  • 2015 IEEE/MTT-S International Microwave Symposium - MTT 2015

    The IEEE MTT-S International Microwave Symposium (IMS) is the premier conference covering basic technologies, to passives and actives components to system over a wide range of frequencies including VHF, UHF, RF, microwave, millimeter-wave, terahertz, and optical. The conference will encompass the latest in RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation, wireless systems, RFID and related topics. The IMS includes technical sessions, both oral and interactive, worksh

  • 2016 IEEE/MTT-S International Microwave Symposium - IMS 2016

    The IEEE International Microwave Symposium (IMS) is the world s foremost conference covering the UHF, RF, wireless, microwave, millimeter-wave, terahertz, and optical frequencies; encompassing everything from basic technologies to components to systems including the latest RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation and more. The IMS includes technical and interactive sessions, exhibits, student competitions, panels, workshops, tutorials, and networking events.

  • 2017 IEEE/MTT-S International Microwave Symposium - IMS 2017

    The IEEE MTT-S International Microwave Symposium (IMS) is the premier conference covering basic technologies, to passives and actives components to system over a wide range of frequencies including VHF, UHF, RF, microwave, millimeter-wave, terahertz, and optical. The conference will encompass the latest in RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation, wireless systems, RFID and related topics.

  • 2018 IEEE/MTT-S International Microwave Symposium - IMS 2018

    Microwave theory and techniques, RF/microwave/millimeter-wave/terahertz circuit design and fabrication technology, radio/wireless communication.

  • 2019 IEEE/MTT-S International Microwave Symposium - IMS 2019

    Comprehensive symposium on microwave theory and techniques including active and passive circuit components, theory and microwave systems.

  • 2029 IEEE/MTT-S International Microwave Symposium - IMS 2029

    The IEEE International Microwave Symposium (IMS) is the world s foremost conference covering the UHF, RF, wireless, microwave, millimeter-wave, terahertz, and optical frequencies; encompassing everything from basic technologies to components to systems including the latest RFIC, MIC, MEMS and filter technologies, advances in CAD, modeling, EM simulation and more. The IMS includes technical and interactive sessions, exhibits, student competitions, panels, workshops, tutorials, and networking events.


2020 IEEE 23rd International Conference on Information Fusion (FUSION)

The International Conference on Information Fusion is the premier forum for interchange of the latest research in data and information fusion, and its impacts on our society. The conference brings together researchers and practitioners from academia and industry to report on the latest scientific and technical advances.


2019 IEEE Aerospace Conference

The international IEEE Aerospace Conference is organized to promote interdisciplinaryunderstanding of aerospace systems, their underlying science, and technology


2019 IEEE/AIAA 38th Digital Avionics Systems Conference (DASC)

To provide a forum for free discussions of new ideas, research, development and applications in order to stimulate and inspire pioneering work in the field of digital avionics and related areas.To acquire high quality technical papers for publication in a DASC Proceedings and other appropriate publications such as the AIAA Journal of Aircraft and IEEE Systems Magazine.To provide a meeting that will further the progress of AIAA and IEEE entities, including Societies, Technical Committees and local Sections and thereby better serve the interests of all AIAA and IEEE members and the community at large.To provide an atmosphere that strengthens the interpersonal rapport of a large number of engineers and scientists interested in specialized and closely related fields.To provide an exhibition of current hardware and software products, methods and tools.To provide instruction in advances in digital avionics and to encourage and reward student academic participation.


2019 IEEE 69th Electronic Components and Technology Conference (ECTC)

premier components, packaging and technology conference



Periodicals related to Aeronautical And Space Sensor Systems

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Advanced Packaging, IEEE Transactions on

The IEEE Transactions on Advanced Packaging has its focus on the modeling, design, and analysis of advanced electronic, photonic, sensors, and MEMS packaging.


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.


Components and Packaging Technologies, IEEE Transactions on

Component parts, hybrid microelectronics, materials, packaging techniques, and manufacturing technology.


Electronics Packaging Manufacturing, IEEE Transactions on

Design for manufacturability, cost and process modeling, process control and automation, factory analysis and improvement, information systems, statistical methods, environmentally-friendly processing, and computer-integrated manufacturing for the production of electronic assemblies, products, and systems.


Nuclear Science, IEEE Transactions on

All aspects of the theory and applications of nuclear science and engineering, including instrumentation for the detection and measurement of ionizing radiation; particle accelerators and their controls; nuclear medicine and its application; effects of radiation on materials, components, and systems; reactor instrumentation and controls; and measurement of radiation in space.



Most published Xplore authors for Aeronautical And Space Sensor Systems

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Xplore Articles related to Aeronautical And Space Sensor Systems

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Passive Wireless Sensor Applications for NASA’s Extreme Aeronautical Environments

IEEE Sensors Journal, 2014

NASA aeronautical programs require rigorous ground and flight testing. Many of the testing environments can be extremely harsh. These environments include cryogenic temperatures and high temperatures (>1500 °C). Temperature, pressure, vibration, ionizing radiation, and chemical exposure may all be a part of the harsh environment found in testing. This paper presents a survey of research opportunities for universities and industry ...


Space debris removal using an automated capturing and self stabilizing system, C.L.E.O.

2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 2017

C.L.E.O. (Cleaner of Lower Earth Orbit) is a space architecture concept that aims at removing debris, ranged between 1 to 10 cm and even larger in diameter. The module consists of two systems; the capturing mechanism and module stabilization. The oncoming debris will be identified using MWIR sensors. Due to the rotatory tendency of the debris, algorithms are used which ...


Low-cost, dual-mode enhanced vision sensor prototype

IEEE Aerospace and Electronic Systems Magazine, 2006

As a member of the Southeast SATSLab Consortium and participant in the NASA Small Aircraft Transportation System (SATS) program, the Rockwell Collins Advanced Technology Center has developed a flyable prototype of a low-cost, dual-mode enhanced vision sensor (EVS). The prototype has been successfully flown on Embry-Riddle Aeronautical University's experimental Cessna 310 light twin aircraft. The dual-mode system incorporates an uncooled ...


Occupancy sensors in carpark based on wireless network

2008 9th International Conference on Signal Processing, 2008

To provide accurate, real time carpark space information, a novel berth detector system which is based on the vortex detection principle, and using wireless technology is designed for the parking guidance system. The berth- detecting algorithm is proposed according to the complicated practical carpark situation via threshold method. The median filter technology is adopted in this algorithm to eliminate transient-upset ...


Sensor blending for direct adaptive control of non-minimum phase linear infinite-dimensional systems in Hilbert space

2017 American Control Conference (ACC), 2017

Linear infinite dimensional systems are described by a closed, densely defined linear operator that generates a continuous semigroup of bounded operators on a general Hilbert space of states and are controlled via a finite number of actuators and sensors. Many distributed applications are included in this formulation, such as large flexible aerospace structures, adaptive optics, diffusion reactions, smart electric power ...



Educational Resources on Aeronautical And Space Sensor Systems

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IEEE.tv Videos

IEEE Region 5 Presents Stepping Stone Awards on the 50th Anniversary of Apollo 11
Supporting IEEE's Mission via Ethical Considerations of Technology | IEEE TechEthics Virtual Panel
Intelligent Systems for Deep Space Exploration: Solutions and Challenges - Roberto Furfaro
Generation of Models for Wireless Sensor Network Assessment
IROS TV 2019-STAR LAB at the University of Surrey Space Technology for Autonomous systems & Robotics
Multiple Sensor Fault Detection and Isolation in Complex Distributed Dynamical Systems
A 4x4x4 mm³ Fully Integrated Sensor-to-Sensor Radio - Li-Xuan Chuo - RFIC 2019 Showcase
NeXOS: Observations Supporting Ocean Sustainability
Collection, Modeling & Interpretation of Mobile Sensor Big Data - Santosh Kumar - IEEE EMBS at NIH, 2019
Robotics History: Narratives and Networks Oral Histories: Gary Bradsky
Large UAS Support: Non Terrestrial Networks - Dallas Brooks - B5GS 2019
Power Electronics for the Space Exploration Hype: APEC 2019
Honors 2020: Byrana N. Suresh & K. Sivan Win the IEEE Simon Ramo Medal
GEOSS for BIODIVERSITY -A demonstration of the GEOSS Common Infrastructure capabilities
Fragility of Interconnected Cyber-Physical Systems - Marios M. Polycarpou - WCCI 2016
IMS 2015: Inkjet-Printed Nanotechnology-Enabled Zero-Power Wireless Sensor Nodes for Smart Skin Applications
2013 IEEE Simon Ramo Medal
MicroApps: Simulation of Airborne, Space-Borne and Ship-Based Radar Systems with Complex Environment (Agilent EEsof)
Localization Services for Online Common Operational Picture and Situation Awareness
ASC-2014 SQUIDs 50th Anniversary: 1 of 6 Arnold Silver

IEEE-USA E-Books

  • Passive Wireless Sensor Applications for NASA’s Extreme Aeronautical Environments

    NASA aeronautical programs require rigorous ground and flight testing. Many of the testing environments can be extremely harsh. These environments include cryogenic temperatures and high temperatures (>1500 °C). Temperature, pressure, vibration, ionizing radiation, and chemical exposure may all be a part of the harsh environment found in testing. This paper presents a survey of research opportunities for universities and industry to develop new wireless sensors that address anticipated structural health monitoring and testing needs for aeronautical vehicles. Potential applications of passive wireless sensors for ground testing and high-altitude aircraft operations are presented. Some of the challenges and issues of the technology are also presented.

  • Space debris removal using an automated capturing and self stabilizing system, C.L.E.O.

    C.L.E.O. (Cleaner of Lower Earth Orbit) is a space architecture concept that aims at removing debris, ranged between 1 to 10 cm and even larger in diameter. The module consists of two systems; the capturing mechanism and module stabilization. The oncoming debris will be identified using MWIR sensors. Due to the rotatory tendency of the debris, algorithms are used which will find the size, shape and angle of approach of the debris with the help of tracking sensors (reducing the error margin to nearly zero). The mechanism chases the debris in the desired orbit by capturing it using the differences in the relativistic motion between the debris and the module and reduces it to near zero. This module can align itself to any object within specified range for straight level entry through set conic angle determined by simulations. C.L.E.O houses a set of reaction wheels for stability and balancing about all the axes, foreseeing any translations due to disturbances to the satellite. This mechanism aims for creating an economical standalone and self-sustaining system that can help in removal, mitigation and control of space junk.

  • Low-cost, dual-mode enhanced vision sensor prototype

    As a member of the Southeast SATSLab Consortium and participant in the NASA Small Aircraft Transportation System (SATS) program, the Rockwell Collins Advanced Technology Center has developed a flyable prototype of a low-cost, dual-mode enhanced vision sensor (EVS). The prototype has been successfully flown on Embry-Riddle Aeronautical University's experimental Cessna 310 light twin aircraft. The dual-mode system incorporates an uncooled long wave infrared sensor and a low-light level visible light imager using a common aperture. The system includes a dichroic beamsplitter that provides the same coaxial field of view to both sensors. This paper describes the design, fabrication, sensor performance, and flight test results of the enhanced vision sensor prototype

  • Occupancy sensors in carpark based on wireless network

    To provide accurate, real time carpark space information, a novel berth detector system which is based on the vortex detection principle, and using wireless technology is designed for the parking guidance system. The berth- detecting algorithm is proposed according to the complicated practical carpark situation via threshold method. The median filter technology is adopted in this algorithm to eliminate transient-upset signal. The wireless module is both used in each detector and the center of the data management to build an data-transferring road. The results show that the vortex berth detector has strong robustness under rapid time-varying temperature condition, and the algorithm is efficient and reliable.

  • Sensor blending for direct adaptive control of non-minimum phase linear infinite-dimensional systems in Hilbert space

    Linear infinite dimensional systems are described by a closed, densely defined linear operator that generates a continuous semigroup of bounded operators on a general Hilbert space of states and are controlled via a finite number of actuators and sensors. Many distributed applications are included in this formulation, such as large flexible aerospace structures, adaptive optics, diffusion reactions, smart electric power grids, and quantum information systems. Using a new normal form for these systems, we have developed the following stability result: an infinite dimensional linear system is Almost Strictly Dissipative (ASD) if and only if its high frequency gain CB is symmetric and positive definite and the open loop system is minimum phase, i.e. its transmission zeros are all exponentially stable. In this paper, we focus on infinite dimensional linear systems that are non-minimum phase and how we can make them minimum phase systems without complicated modifications. First we will show that the zeros are invariant under coordinate transformations and both static and dynamic feedback. So our only choice will be to modify the input-output operators B & C. This is called sensor (or actuator) blending. Our principal result will be a systematic way to do sensor blending on an infinite dimensional linear system with a finite number of unstable zeros. These results will be illustrated by application to direct adaptive control of general linear systems on a Hilbert space that are described by self-adjoint operators with compact resolvent.

  • Fault-tolerant controller design for one hypersonic aircraft with sensor failure

    Compared with traditional aircraft, the near space hypersonic aircraft control system has a very prominent strong coupling, strong nonlinear, time-varying dynamics characteristics. In its research and design process, the following factors must be considered: plant elastic deformation, multi-inputs multi- outputs, aerodynamatic parameters uncertain, and a variety of temperature sensor failure and other causes of fever and some actuator failures and other issues, so the research and design of aircraft control systems faces unprecedented difficulties and challenges of the Institute. To solve the angular rate sensor failure problems encountered for hypersonic aircraft during flight, the nonlinear observer and controller are designed respectively. Under the condition of output measureable only, the dissertation designs a new standard expanded Luenberger observer to estimate convergence state vector, and brings forward a new strong adaptive control law based on dynamic surface adaptive backstepping control to guarantee the system boundedness. In the course of adaptive backstepping design, the dissertation employes the dynamic surface control strategy to eliminate the traditional inversion of the "dimesion explosion" question by introducing a series of first order filters to obtain the differentiation of the virtual control inputs. The six degrees of freedom simulation of hypersonic aircraft is used to verify the above theory.

  • Low-cost, dual-mode enhanced vision sensor prototype

    As a member of the Southeast SATSLab Consortium and a participant in the NASA small aircraft transportation system (SATS) program, the Rockwell Collins Advanced Technology Center has developed a flyable prototype of a low-cost, dual-mode enhanced vision sensor (EVS). The prototype has been successfully flown on Embry-Riddle Aeronautical University's experimental Cessna 310 light twin aircraft. The dual-mode system incorporates an uncooled long wave infrared sensor and a low light level visible light imager using a common aperture. The system includes a novel dichroic beamsplitter that provides the same coaxial field of view to both sensors. This paper describes the design, fabrication, sensor performance, and flight test results of the enhanced vision sensor prototype.

  • Space Surveillance Network and Analysis Model (SSNAM) Performance Improvements

    The space surveillance network and analysis model (SSNAM) is an air force space command (AFSPC) model, which provides the capability to analyze and architect space surveillance network (SSN) force structure. To provide these capabilities SSNAM supports two types of simulations: catalog maintenance, and special events (launch, on-orbit events, and breakup). There are many configuration options available with SSNAM: models for all the sensors currently in the SSN to include space based and ground based sensors, hours of operation by sensor, track capacity by sensor, models for sensors yet to be created, user defined weather conditions, National Aeronautical and Space Administration catalog growth model including space debris, and solar flux just to name a few. SSNAM is a large software system. It is written in Java, C/C++, and FORTRAN (77 & 95), represents over a million lines of code, and employs a Web-based, load-sharing architecture to decrease simulation runtime. Catalog maintenance simulations are both computationally and input/output (I/O) intensive. A typical catalog maintenance simulation (10 K to 35 K satellites simulated over a 90 day period) will generate over a terabyte of data, during the course of a simulation, which is reduced down to approximately 1.5 gigabytes. Depending on simulation configuration, runtimes can range from 12 to 48 hours on a 16 node, PC network cluster. Because of the high computational demands of SSNAM catalog maintenance simulations and the anticipation of transitioning SSNAM to model the maintenance of an special perturbation (SP) catalog, the SSNAM system was ported to run on Maui High Performance Computing Center (MHPCC) platforms. This port resulted in at least a three-fold increase in performance for all currently parallelized processing in SSNAM. This paper provides an overview of the SSNAM application, its Web based, load sharing architecture, the effort involved with porting Java and FORTRAN to MHPCC platforms, the approach and implementation for parallelizing the SP tasker, and the resulting performance gains.

  • Bluetooth Low Energy based inertial sensors test and verification tool

    The development of Micro-Electro-Mechanical Systems based inertial sensors is the basis of an increasing number of commercial and scientific solutions for unmanned vehicles aeronautical/aerospace navigation systems and health and sports monitoring solutions. Inertial sensors widespread use within embedded systems also prompted the development of algorithms to cope with their inherent inaccuracy. These sensors, with small form factor and low cost, present an advantage for computing three-dimensional space object orientation. Also radio frequency communication devices are frequently associated with inertial sensors and embedded systems. Radio frequency communication protocols allow immediate data transfer and processing without cumbersome cabling. This work proposes a Bluetooth Low Energy based framework to evaluate the behavior of inertial sensors fusion algorithms. A Yaskawa Motoman NX100 robotic arm has been used to implement a set of predefined movements that granted the mandatory test accuracy and repeatability conditions. The Bluetooth Low Energy device has been implemented to transfer the inertial sensor data to a PC computer running a Windows operating system. The inertial sensors have been implemented with a MPU-9150 Inertial Measurement Unit (IMU) that includes an accelerometer, a gyroscope and a compass. The proposed framework has been used to test and verification of a number of sensor fusion algorithms.

  • Pulsed eddy current imager for the enhanced non destructive evaluation of aeronautical riveted assemblies

    In this paper, an original pulsed eddy current (EC) imaging system dedicated to the enhanced non-destructive evaluation (NDE) of aeronautical riveted is presented. The system aims to combine the advantages of the pulsed eddy current (PEC) sensors with those of EC imaging devices. The system is based on the combination of a PEC inducer, and a magneto-optical (MO) set-up used to measure the magnetic two-dimensional impulse response of the part under evaluation. The obtained data are in the form of a temporal succession of high resolution EC images, enabling both the spatial and temporal EC characterization of the part. The system is implemented here on aluminum riveted assemblies featuring calibrated defects placed next to rivets. The study demonstrates the relevance of the PEC imager to separate defects signature from rivets and to characterize the detected defects thanks to the extraction of space-time features from the provided data.



Standards related to Aeronautical And Space Sensor Systems

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IEEE Recommended Practice for Inertial Sensor Test Equipment, Instrumentation, Data Acquisition, and Analysis

Recommended practices for gyroscope and accelerometer testing are discussed, ranging from the equipment and instrumentation employed to the way that tests are carried out and data are acquired and analyzed.


IEEE Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers

Generate errata and/or revisions to the existing Std. 836-1991.


IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros


IEEE Specification Format Guide and Test Procedure for Two-Degree-of-Freedom Dynamically Tuned Gyros


IEEE Standard for Inertial Sensor Terminology

To review all of the definitions included in the standard and to revise them as required. New terminology will be added to bring the document up to date with current technology.