With the continuous enrichment and development of power business types and quantities, as well as the pilot application of domestic databases and self-developed databases, the database type of State Grid Corporation o...
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As an important component of the intelligent machinery field, desktop robots not only enrich people's entertainment lives but are also gradually expanding into applications in education, healthcare, and other fiel...
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This paper investigates usability aspects of a mobile application aimed at monitoring symptoms of Parkinson's disease (PD) patients. Thirty PD patients collected data through mobile-based questionnaires and activi...
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This study addresses the requirements for tank inerting and proposes application-oriented architectures for inert gas distribution system. Utilizing AMEsim, a multi-tank simulation model is constructed. The accuracy o...
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This study is based on the current development status of existing amphibious flying robots and identifies their design shortcomings. A new industrial prototype design for amphibious flying robots suitable for water, l...
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ISBN:
(纸本)9798350373141;9798350373158
This study is based on the current development status of existing amphibious flying robots and identifies their design shortcomings. A new industrial prototype design for amphibious flying robots suitable for water, land, and air use has been proposed. Through a detailed analysis of overall parameters, external structure, wing layout and transformation, shape transformation control, takeoff and landing methods, and power systems, this study aims to achieve a compact and stable robot design to ensure good manoeuvrability and adaptability in different environments. Meanwhile, by adopting a variable wing design and an efficient shape transformation control system, the robot can achieve optimized aerodynamic performance and smooth, fast shape transformation in different flight modes. In addition, diversified takeoff and landing methods are proposed, such as vertical takeoff and landing, horizontal takeoff and landing, etc., to meet diverse task requirements. Finally, a design combining advanced electric and fuel power systems is adapted to meet the long-term flight requirements in different environments. Through these detailed analyses, this study provides important references for the further development and application of amphibious flying robots suitable for water, land, and air use.
Breast cancer is a leading cause of cancer-related deaths among women worldwide. Continuously monitoring of breast state is critical for effective treatment and improved patient outcomes. In this work, we propose a de...
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Most tasks in airborne scenarios are composed of neural networks (NN) and non-NN tasks. On the one hand, Deep neural networks (DNNs) have become the mainstream method of AI task processing. DNNs is accompanied by a la...
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When we define a large-scale system, a typical example would be a space development project. When we talk about large-scale systems in space development, there is the international Space Station (ISS), which was propo...
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ISBN:
(纸本)9798350380040
When we define a large-scale system, a typical example would be a space development project. When we talk about large-scale systems in space development, there is the international Space Station (ISS), which was proposed by NASA in the 1980s as a manned space station, and which Japan, ESA, Canada, and later Russia joined as international partners. Japan's unique space transportation system, rocket development, began in the 1970s, and has a history of development of the H-1, H-2, and the new H-3, making it a largescale system promoted by Japan. In addition, the satellite carried on the third H-3 is called ALOS-4, which has an earth observation mission, and is a large satellite that weighs 3 tons and is 20 meters long when the solar paddles are deployed, so it can be said to be a large-scale system. In this paper, the author looks back on and explains the integration and verification of the international Space Station from development to operation, focusing on the development of large-scale space power systems, their integration, and verification. In addition, from a comparative perspective, the integration and verification of Japanese rocket development is compared with the ISS. The conceptual and basic design of the international Space Station began in the 1980s, and in-orbit assembly began in 1998. It is scheduled to be completed in 2011 and to end its role in 2030. Looking back at the history of the ISS, there are broadly a design phase, a development phase, and an assembly phase, and the operation phase began after in-orbit assembly began. In these phases, test verification and integration tests were conducted according to the phase at that time. The international Space Station, a large-scale space system, initially had an extremely high-risk assembly scenario in which elements and modules from each country were launched, connected in orbit, and element-to-element integration and verification tests were conducted for the first time. In this paper, the author desc
With technological advancement and based on the principle of Communication of objects, oriented applications towards intelligent energy management are in line to be the simplest, most effective, while allowing to prov...
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For the fast steering mirror system used for beam pointing control, in order to ensure that the fast steering mirror can work stably under high bandwidth, this paper proposes a design method of the current loop drive ...
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