Performance-Guaranteed Attitude Tracking Control for RLV: A Finite-Time PPC Approach-Reference-Cited by-同舟云学术

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Performance-Guaranteed Attitude Tracking Control for RLV: A Finite-Time PPC Approach

Published:2024-08 Issue:4 Volume:60 Page:5024-5034
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Guo Zongyi¹^ORCID,Henry David²^ORCID,Gu Xiyu³^ORCID,Ygorra Stephane⁴,Cieslak Jérôme⁴^ORCID,Guo Jianguo¹^ORCID

Affiliation:

1. Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi'an, China

2. University of Bordeaux, Talence, France

3. Department of Information Engineering, University of Padova, Padua, Italy

4. IMS-Lab, University of Bordeaux, Talence, France

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/7/10631738/10494344.pdf?arnumber=10494344

Reference40 articles.

1. Overview of reusable space systems with a look to technology aspects

2. Lectures about Buran and the recent MAKS re-entry;Bushgens,1999

3. Space shuttle entry terminal area energy management;Moore,1991

4. Advanced flight control issues for reusable launch vehicle;Bavacqua,2004

5. New Nonlinear Control Technique for Ascent Phase of Reusable Launch Vehicles

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