11,319 resources related to Aerospace Control
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2021 IEEE Photovoltaic Specialists Conference (PVSC)
Photovoltaic materials, devices, systems and related science and technology
The ACC is the annual conference of the American Automatic Control Council (AACC, the U.S. national member organization of the International Federation for Automatic Control (IFAC)). The ACC is internationally recognized as a premier scientific and engineering conference dedicated to the advancement of control theory and practice. The ACC brings together an international community of researchers and practitioners to discuss the latest findings in automatic control. The 2020 ACC technical program will
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.
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
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.
The IEEE Aerospace and Electronic Systems Magazine publishes articles concerned with the various aspects of systems for space, air, ocean, or ground environments.
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.
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
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 ...
The IEEE Transactions on Automation Sciences and Engineering (T-ASE) publishes fundamental papers on Automation, emphasizing scientific results that advance efficiency, quality, productivity, and reliability. T-ASE encourages interdisciplinary approaches from computer science, control systems, electrical engineering, mathematics, mechanical engineering, operations research, and other fields. We welcome results relevant to industries such as agriculture, biotechnology, healthcare, home automation, maintenance, manufacturing, pharmaceuticals, retail, ...
IEE Colloquium on Integrating Issues in Aerospace Control, 1991
2006 ieee/aiaa 25TH Digital Avionics Systems Conference, 2006
Tight government budget constraints and a rapid technological change contributed to the development of the modular open systems approach (MOSA) as an integrated business and engineering strategy. Such an approach to acquisition makes it possible to leverage the achievements of commercial industries for an effective integration of subsystems and systems. Companies involved in government programs are asked to actively research ...
Proceedings of the 31st Chinese Control Conference, 2012
Telemetry data-driven 3D visualization can help flight controllers decision in space measurement and control tasks, which has a very important significance. But the telemetry usually causes an abnormal value in measuring and translation. Moreover, we can't get telemetry when the spacecraft is out of measuring and controlling network. We provide a comprehensive telemetry processing method to obtain continuous stability data, ...
IEEE Conference on Aerospace Applications, 1990
The author reviews the requirements placed on the controller in real-time aerospace control applications and compares them with those found in the digital signal processing (DSP) field. The application of a family of powerful DSP microchips to the field of aerospace control systems is studied. An example of a simple control system is used to present the basic concepts and ...
Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference, 2014
According to the characteristics of lunar orbiter tracking, a novel automotive navigation method based on camera and laser altimeter was proposed. It is aided by historic images and terrain features as to enhance the autonomy of aerospace control. The prototype of the method was studied, and the key technologies was analyzed. Cameras obtain real-time images of the lunar surface, while ...
Shaping the Future of Quantum Computing - Suhare Nur - ICRC San Mateo, 2019
The AcceleGlove: A Cheap and Lightweight Control Glove
IEEE Magnetics Distinguished Lecture - Alison B. Flatau
Engineering Our Future - Randii R. Wessen, Ph.D
IROS 2014 Plenary: Andrew Davison
Key Technology Trends in Wireless for the Aerospace Industry
Bill Woodward presents NEEDLES: 2016 End to End Trust and Security Workshop for the Internet of Things
Performance Analytics, Valuation Trends & the M&A Market
Pat Wheeler, Distinguished Lecturer
Inspiring Brilliance: The impact of control theory and cybernetics of Maxwell's paper: On governors
Optimization for Robust Motion Planning and Control
The Full Spectrum: Travelogue of the Atomic Age
Navigation and Control of Unmanned Vehicles: A Fuzzy Logic Perspective
ICRA Keynote: Dr. Shigeo Hirose
IROS 2014 Plenary: Todd Kuiken
Q-Band CMOS Transmitter System-on-Chip - Tim Larocca - RFIC Showcase 2018
EMBC 2011-Workshop-Motor Control Principles in Neurorobotics and Prosthetics-PT IV
IEEE PES Awards 2020: IEEE PES Prabha S. Kundur Power System Dynamics and Control Award
100 Years of IEEE and Aerospace - An Oral History
Tight government budget constraints and a rapid technological change contributed to the development of the modular open systems approach (MOSA) as an integrated business and engineering strategy. Such an approach to acquisition makes it possible to leverage the achievements of commercial industries for an effective integration of subsystems and systems. Companies involved in government programs are asked to actively research and analyze the market to identify the technologies, standards, and compliant products for the design of open systems. In the scope of the formal acquisition processes, contractors should evaluate the total lifecycle costs and build a business case for using off-the-shelf technologies, existing standards and open architectures, where feasible and appropriate. Key drivers for such decisions are evolving capability requirements and anticipated technological change over the lifecycle of the system. At present, the increase in operation and support costs of avionics systems can be attributed to insufficient standardization and reduced capability for incremental modernization of available systems. In general MOSA can help to reduce development cycles time and product support costs within an evolutionary acquisition context. It facilitates system engineering for affordable reconfiguration, modernization, and change. From 2004, DoDD 5000.1 directs all acquisition programs to employ MOSA as part of systems engineering (Azani et al., 2005). This paper examines the compliance of time-triggered protocol (TTP), as a technology platform for advanced integrated aerospace control systems, with modular open system approach (MOSA)
Telemetry data-driven 3D visualization can help flight controllers decision in space measurement and control tasks, which has a very important significance. But the telemetry usually causes an abnormal value in measuring and translation. Moreover, we can't get telemetry when the spacecraft is out of measuring and controlling network. We provide a comprehensive telemetry processing method to obtain continuous stability data, driving the 3d visualization outputting. Practice of the first rendezvous and docking mission showed that the handling method is a practical and reliable method of engineering.
The author reviews the requirements placed on the controller in real-time aerospace control applications and compares them with those found in the digital signal processing (DSP) field. The application of a family of powerful DSP microchips to the field of aerospace control systems is studied. An example of a simple control system is used to present the basic concepts and to show the effects of data sampling rate. The code sequence required to implement the control law is shown for a floating-point DSP microchip, and the timing is also given. It is concluded that DSP microchips, such as the Motorola DSP56001 and DSP96002, are extremely powerful and have the speed necessary for real-time control applications. Their instruction sets easily meet the requirements for real-time operating systems. Fixed-point units, such as the DSP56001 with 24-b precision, are more than adequate for many applications. For complicated control systems, like those using Kalman filtering to predict the state of the system, DSP microchips with floating- point capability, such as the 32-b DSP96002, would be the logical choice, for they increase dynamic range and are much easier to use.<<ETX>>
According to the characteristics of lunar orbiter tracking, a novel automotive navigation method based on camera and laser altimeter was proposed. It is aided by historic images and terrain features as to enhance the autonomy of aerospace control. The prototype of the method was studied, and the key technologies was analyzed. Cameras obtain real-time images of the lunar surface, while laser altimeter provides real-time orbital altitude. The altitude data can be introduced to get the resolution of the real-time image, in case camera may bring a series of uncertainties because the orbiter's altitude changes with the lunar gravity anomaly and topography. This is good for the reliability of image matching. The method of solving the position and attitude of the orbiter is given. The sufficiency and advantages of this method are also discussed.
Chang'E-2(CE-2) extended mission started from June 2011, the maximum distance between CE-2 and the Earth is about 1,700,000 km. In this paper, orbit determination for CE-2 extended mission is discussed, and the orbit accuracy during transfer orbit phase is assessed. The results show that under current tracking condition, the orbit accuracy during the early escape orbit phase is at the level of 1km. As the distance increases, longer arc-length is needed for orbit determination. During the later transfer orbit phase, orbit determination was performed using more than 20-day tracking data, and the orbit accuracy is better than 2km.
Manned space flight control mission has the features of technology complexity, high requirement of reliability and real time, enormousness of software and hardware system, and difficulty in flight control cooperation, aiming at which this paper presents an Integrative Flight Control Validation (IFCV) architecture. The validation environment is composed of the actual spacecraft, astronauts, the software and hardware for mission in tracking station and flight control center. Before the launch of manned spacecraft, the IFCV implements comprehensive validation of the interface of spacecraft and ground system, the normal and emergency program for mission, the countermeasures against various faults, and the cooperation process between astronauts, spacecraft and ground system. Through maximizing the scope and reality of flight control validation, the preparative time is shortened, the hidden trouble is eliminated and the success of manned spacecraft mission is guaranteed.
Reusable Booster Vehicles(RBV) is a new type of Two-Stage-To-Orbit(TSTO) partly reusable launch vehicle, which can greatly reduce launch cost. The guidance control during the reentry period of RBV is critical for safe and reliable return. In order to satisfy special task demands, this paper has analyzed the performance of neural network guidance, normal trajectory guidance and prediction-correction guidance, and given related comparison conclusions. The neural network has been trained according to the trajectory parameters generated by using prediction-correction guidance method. The state parameters of RBV have been used as the input, and the bank angle has been the output. Simulation result has indicated that the proposed method has good real time performance and its computation occupation is low. What's more, it also has good robustness and adaption performance by using the proposed method. In the case of larger initial bias or greater error of RBV pneumatic parameters, it could attain good land precision. It has a very good application future by utilizing the reentry guidance method for RBV based on neural network.
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