Direct trajectory optimization framework for vertical takeoff and vertical landing reusable rockets: case study of two-stage rockets-Reference-Cited by-同舟云学术

Direct trajectory optimization framework for vertical takeoff and vertical landing reusable rockets: case study of two-stage rockets

Published:2018-07-04 Issue:4 Volume:51 Page:627-645
ISSN:0305-215X
Container-title:Engineering Optimization
language:en
Short-container-title:Engineering Optimization

Author:

Ma Lin¹,Wang Kexin¹,Shao Zhijiang¹,Song Zhengyu²,Biegler Lorenz T.³

Affiliation:

1. College of Control Science and Engineering, Zhejiang University, Hangzhou, People's Republic of China

2. Beijing Aerospace Automatic Control Institute, Beijing, People's Republic of China

3. Department of Chemical Engineering, Carnegie Mellon University, Pittsburgh, PA, USA

Funder

National Nature Science Foundation of China

Equipment Pre-Research Project of China

Joint Innovation Fund of the China Academy of Launch Vehicle Technology and Universities

Fundamental Research Funds for the Central Universities

State Key Laboratory Project of China

Publisher

Informa UK Limited

Subject

Applied Mathematics,Industrial and Manufacturing Engineering,Management Science and Operations Research,Control and Optimization,Computer Science Applications

Link

https://www.tandfonline.com/doi/pdf/10.1080/0305215X.2018.1472774

Reference32 articles.

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3. Convex Programming Approach to Powered Descent Guidance for Mars Landing

4. Benson, D. 2005. “A Gauss Pseudospectral Transcription for Optimal Control.” Ph.D. Dissertation, Massachusetts Institute of Technology, Cambridge, MA.

5. Direct Trajectory Optimization and Costate Estimation via an Orthogonal Collocation Method

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