Integrated elastic identification and LOS angular rate extraction for slender rockets: A continuous-discrete maximum correntropy Kalman filter approach-Reference-Cited by-同舟云学术

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Integrated elastic identification and LOS angular rate extraction for slender rockets: A continuous-discrete maximum correntropy Kalman filter approach

Published:2024-07 Issue: Volume:150 Page:109174
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Duo^ORCID,Song Jianmei,Zhu Yeqing^ORCID,Jiao Tianfeng,Zhao Liangyu^ORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference34 articles.

1. Autonomous trajectory generation algorithms for spacecraft slew maneuvers;Sandberg;Aerospace,2022

2. Autonomous trajectory generation comparison for de-orbiting with multiple collision avoidance;Raigoza;Sensors,2022

3. Solving multiobjective constrained trajectory optimization problem by an extended evolutionary algorithm;Chai;IEEE Transactions on Cybernetics,2020

4. Real-time reentry trajectory planning of hypersonic vehicles: a two-step strategy incorporating fuzzy multiobjective transcription and deep neural network;Chai;IEEE Transactions on Industrial Electronics,2020

5. Controlling remotely operated vehicles with deterministic artificial intelligence;Osler;Applied Sciences,2022

Cited by 1 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. Fault-Tolerant Integrated Guidance and Control Design for the Flight Vehicle without LOS Angular Rate Measurement;Applied Sciences;2024-09-12

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