Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costates-Reference-Cited by-同舟云学术

Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costates

Published:2019-03 Issue:3 Volume:42 Page:585-597
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,Li Shuang¹,Bai Xiaoli²

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

2. Rutgers University, Piscataway, New Jersey 08854

Funder

Innovation Funded Project of Shanghai Aerospace Science and Technology

Scientific Research Foundation for New Staffs of Nanjing University of Aeronautics and Astronautics

National Natural Science Foundation of China

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

https://arc.aiaa.org/doi/pdf/10.2514/1.G003414

Reference28 articles.

1. System design of the Hayabusa 2—Asteroid sample return mission to 1999 JU3

2. LantoineG.BraunR. D. “Optimal Trajectories for Soft Landing on Asteroids,” AE8900 MS Special Problems Rept., Space Systems Design Lab. Georgia Inst. of Technology, Atlanta, GA, Dec. 2006, http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.217.2875 [retrieved 07 Oct. 2018].

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

4. Autonomous navigation and guidance for landing on asteroids

5. Finite-time soft landing on asteroids using nonsingular terminal sliding mode control

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