Rapid Generation of Time-Optimal Trajectories for Asteroid Landing via Convex Optimization-Reference-Cited by-同舟云学术

Rapid Generation of Time-Optimal Trajectories for Asteroid Landing via Convex Optimization

Published:2017-03 Issue:3 Volume:40 Page:628-641
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Yang Hongwei¹,Bai Xiaoli²,Baoyin Hexi¹

Affiliation:

1. Tsinghua University, 100084 Beijing, People’s Republic of China

2. Rutgers University, Piscataway, New Jersey 08854

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G002170

Reference32 articles.

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3. LantoineG.BraunR. D. “Optimal Trajectories for Soft Landing on Asteroids,” Space Systems Design Lab. Georgia Inst. of Technology, AE8900 MS Special Problems Rept., Atlanta, Dec. 2006.

4. An autonomous optical navigation and guidance for soft landing on asteroids

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