Design Method for Landing Gear Mechanisms Based on Characterization Matrix
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-8045-1_14
Reference8 articles.
1. Udayakumar R, Ibrahim M (2019) Design analysis of landing gear system of an aircraft. In: 2019 3rd International conference on electronics, communication and aerospace technology. India, pp 1326–1330
2. Douglas C, et al (2021) Multidisciplinary design optimization of aircraft landing gear. AIAA AVIATION 2021 FORUM
3. Zhu L, Zou Z, Yin Y et al (2021) Intelligent design method of landing gear retraction and extension trajectory for narrow space. J Beijing Univ Aeronaut Astronaut 47(12):2560–2570
4. Ye Y, et al (2023) Intelligent optimization of landing gear retraction based on physical simulation. J Phys Conf Ser 2469(1) (IOP Publishing)
5. Chen H, Yuhong J (2018) Optimal design of aircraft landing gear mechanism actuating force. In: 2018 3rd Joint international information technology, mechanical and electronic engineering conference (JIMEC 2018). Atlantis Press
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