Online Trajectory Optimization Method for Large Attitude Flip Vertical Landing of Starship-like Vehicles-Reference-Cited by-同舟云学术

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Online Trajectory Optimization Method for Large Attitude Flip Vertical Landing of Starship-like Vehicles

Published:2022-10-28 Issue: Volume: Page:
ISSN:
Container-title:2022 IEEE International Conference on Unmanned Systems (ICUS)
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Author:

Ma Zhenwei¹,Yan Ning²,Wang Jinbo¹,Chen Hongbo¹

Affiliation:

1. School of Systems Science and Engineering, Sun Yat-Sen University,Guangzhou,China

2. China Academy of Launch Vehicle Technology,Research and Development Department,Beijing,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9986510/9986514/09986876.pdf?arnumber=9986876

Reference11 articles.

1. Analysis of SpaceX's “Super Heavy-Starship” transportation system scheme;yan;Space International,2020

2. Analysis of the development of SpaceX's reusable launch vehicle;yang;Space International,2020

3. A brief analysis of the super-heavy-starship transport system and its future impact;long;Aerospace and Technology,2021

4. Development of online trajectory planning technology for launch vehicle return and landing;song;Astronautical Systems Engineering Technology,2019

5. Characteristics of starship propulsion system and numerical simulation of propellant flow during reentry;luo;Journal of NanJing University of Aeronautics and Astronautics,2021

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. Linearized State-Space Model-Based Attitude Control for Rocket With Four Controllable Fins—Part 1-1: Basic Modeling and Identification;IEEE Access;2023

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