Formulation of seven degree of freedom state space model of aircraft with active landing gear-Reference-Cited by-同舟云学术

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Formulation of seven degree of freedom state space model of aircraft with active landing gear

Published:2022 Issue: Volume: Page:
ISSN:0094-243X
Container-title:2ND INTERNATIONAL CONFERENCE ON MATHEMATICAL TECHNIQUES AND APPLICATIONS: ICMTA2021
language:
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Author:

Sivaprakasam Sivakumar,Baskaran Sanjay

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0108428

Reference5 articles.

1. Optimal Active Control of Vehicle Suspension System Including Time Delay and Preview for Rough Roads

2. Active Suspension Control of Eight Degrees of Freedom Vehicle Model

3. Dynamic Analysis of Aircraft Landing Impact Using Landing-Region-Based Model

4. An investigation of an active landing gear system to reduce aircraft vibrations caused by landing impacts and runway excitations

5. Non-linear vibration analysis of oleo pneumatic landing gear at touchdown impact

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Calculation of the Passenger Aircraft Landing Gear Shock Absorption System Exposed to Impact Loading;Herald of the Bauman Moscow State Technical University. Series Mechanical Engineering;2023-09

2. Optimization of the gas-liquid damper pin in the aircraft landing gear;Proceedings of Higher Educational Institutions. Маchine Building;2023-09

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