Titlebook: Aerospace Mechatronics and Control Technology; Selected Contributio Huafeng Ding Conference proceedings 2022 The Editor(s) (if applicable)

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End-to-End Neural Dialogue Systems,l inspection indicator during engine assembly. With the higher demand for consistency of engine performance, the measurability of BTC is required to be much more accurate and dynamically. However, the traditional BTC detection method in the assembly process is restricted to lower accuracy, inability

ACTIN

Statistical Data-Driven Dialogue Systems,athematical model based analysis methods are studied to realize assembly deviation prediction. However, most established analysis methods require abstraction and simplification of geometric deviations, which results in the inability to accurately characterizing the surface deviation features and ana

侵害

Kei Wakabayashi,Johane Takeuchi,Mikio Nakanoproposes a method for online identification and prediction of solid rocket motor performance. The calculation model of the nozzle throat diameter and the propellant burning rate are established based on the analysis of internal correlation between motor parameters. Then by means of the real-time mea

Genistein

Cabinet

https://doi.org/10.1007/978-981-19-5538-9 crucial importance to the system’s imaging quality. However, the mirror shape is usually influenced by gravity, temperature, forced displacement and launch vibrations to distort after leaving earth. The support structure of the subassembly plays an important role to minimize the impact of above fac

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破布

Svetlana Stoyanchev,Stefan Ultes,Haizhou Lia target localization method that combines on-board IMU data and image information. This method does not require equipment such as GPS or optoelectronic platform, nor does it need prior knowledge or templates of the target. Firstly, a selection strategy is proposed to determine keyframes, which are

ureter

Learning to Rank Intents in Voice Assistants attitude updating algorithm of the traditional micro-nano satellite is no longer applicable. This paper proposes a modified attitude updating scheme applied to agile satellites. The method adopts the coning motion as the research scene, in which the influence of noncommutativity error is the worst.

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https://doi.org/10.1007/978-981-16-6640-7Aerospace Mechatronics; Mechanical Engineering; Mechanical Design; Control System; Fluid Mechanics and M