Paper information

Paper code

IAC-18,D2,IP,5,x44659

Order

5

Room

IP Hall

Title

Trajectory Optimization for Powered Descent and Landing of Reusable Rockets with Restartable Engines

abstract

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Session

IP. Interactive Presentations - IAF SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

symposium

D2. IAF SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

congress

IAC-18

Type of presentation

interactive

Main author

Dr. Lin Ma, Zhejiang University, China

Co-authors

Dr. Kexin Wang, Zhejiang University, China;

Prof. Zuhua Xu, Zhejiang University, China;

Prof.Dr. Zhijiang SHAO, Zhejiang University, China;

Prof. Zhengyu Song, China Academy of Launch Vehicle Technology (CALT), China;