Research on Simulation and Optimization of Pulse Controlled Multiple Launch Rocket System
Lecture Notes in Mechanical Engineering, ISSN: 2195-4364, Page: 2273-2283
2024
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Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
Citation Benchmarking is provided by Scopus and SciVal and is different from the metrics context provided by PlumX Metrics.
Conference Paper Description
Multiple Launch Rocket System (MLRS) has been widely used all around the world due to the advantages such as high firing speed, large firing area, long firing range, good mobility and heavy firepower density weaved in a short period time. The Pulse Controlled Multiple Launch Rocket System (PCMLRS) is able to suppress the vibration during launching process by applying the pulse thrusters, which helps improve its dispersion characteristics. In this paper, the system composition of PCMLRS is introduced and the simulation system of PCMLRS is built using the Multibody System Transfer Matrix Method, based on which the pulse control parameters are optimized. The simulation results show that the firing dispersion of PCMLRS is improved, which indicates good engineering application prospects.
Bibliographic Details
http://www.scopus.com/inward/record.url?partnerID=HzOxMe3b&scp=85197341216&origin=inward; http://dx.doi.org/10.1007/978-981-99-8048-2_156; https://link.springer.com/10.1007/978-981-99-8048-2_156; https://dx.doi.org/10.1007/978-981-99-8048-2_156; https://link.springer.com/chapter/10.1007/978-981-99-8048-2_156
Springer Science and Business Media LLC
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