Neuroadaptive high-order fully-actuated system approach for roll autopilot with unknown uncertainties-Reference-Cited by-同舟云学术

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Neuroadaptive high-order fully-actuated system approach for roll autopilot with unknown uncertainties

Published:2024-12 Issue: Volume:155 Page:109567
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Wei,Chen Shiwei,Shi Zhongjiao,Wang Yuchen^ORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference48 articles.

1. Roll instability and control during pitching maneuver for a missile with strake wings;Wang;Acta Aeronaut. Astronaut. Sin.,2016

2. Roll stabilization: a higher-order sliding-mode approach;Trivedi;IEEE Trans. Aerosp. Electron. Syst.,2015

3. Robust optimal sliding mode control of missile autopilot based on adaptive dynamic programming;Tian;Control Decis.,2021

4. A LOS rate estimation method for bank-to-turn missiles;Song;IEEE Trans. Aerosp. Electron. Syst.,2008

5. Adaptive roll control of guided munitions with state independent uncertainty parameterization;Ovec,2017

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