Design and Simulation Verification of Aircraft Altitude Control Based on Hybrid Algorithm-Reference-Cited by-同舟云学术

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Design and Simulation Verification of Aircraft Altitude Control Based on Hybrid Algorithm

Published:2022-10 Issue: Volume: Page:
ISSN:
Container-title:2022 International Symposium on Intelligent Robotics and Systems (ISoIRS)
language:
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Author:

Wang Lingling¹,XinYu Yin¹

Affiliation:

1. Naval Aviation University,Yantai,China,264000

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10196672/10196679/10196696.pdf?arnumber=10196696

Reference5 articles.

1. Fuze Roll Angle Control Based on Bang Bang Rudder[J];pengfei;Journal of Detection & Control,2018

2. Research of Height Control Technique on UAV Automatic Langding[J];kai;Computer Measurement & Control,2016

3. Design and Simulation of Unmanned Aerial Vehicle Height Control System Based on PI [J];dongqing;Control theory and applications,2017

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. Backstepping based High-order Sliding Mode Control for UAV Attitude Tracking;2024 36th Chinese Control and Decision Conference (CCDC);2024-05-25

2. Forming-based geometric correction methods for thin-walled metallic components: a selective review;The International Journal of Advanced Manufacturing Technology;2023-07-24

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