Ascent control of heavy-lift launch vehicle with guaranteed predefined performance-Reference-Cited by-同舟云学术

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Ascent control of heavy-lift launch vehicle with guaranteed predefined performance

Published:2021-03 Issue: Volume:110 Page:106511
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Liang^ORCID,Ju Xiaozhe^ORCID,Cui Naigang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

1. A recovery system for the key components of the first stage of a heavy launch vehicle;Dek;Aerosp. Sci. Technol.,2020

2. Adaptive attitude control for a heavy-lift launch vehicle;Zhang,2019

3. Heavy lift launch vehicle technology of adaptive augmented fault tolerant control;Zhang,2016

4. Modeling and attitude control for strap-on launch vehicle with POGO vibration;Liu,2015

5. Modeling, design and analysis of large strap-on launch vehicle's attitude control system;Li,2011

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2. Approximate analytical solutions for three-dimensional ascent trajectory of a solid-fuel launch vehicle;Chinese Journal of Aeronautics;2024-06

3. A novel predefined performance barrier function based adaptive sliding mode control method for RLV under mismatched disturbance;Aircraft Engineering and Aerospace Technology;2024-05-06

4. Self-Adjusting Prescribed Performance H∞ Trajectory Tracking Control for Underactuated Autonomous Underwater Vehicles;IEEE Access;2024

5. Neural Network Observer-Based Predefined-Time Attitude Control for Morphing Hypersonic Vehicles;2024

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