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

Journal article

Peer reviewed

Hongwei Yang, Shuang Li and Xiaoli Bai

Journal of guidance, control, and dynamics, Vol.42(3), pp.585-597

03/2019

Metrics

19 Record Views

Title: Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costates
Creators: Hongwei Yang - Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Shuang Li - Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Xiaoli Bai - Rutgers University, Piscataway, New Jersey 08854
Publication Details: Journal of guidance, control, and dynamics, Vol.42(3), pp.585-597
Date published: 03/2019
Academic Unit: Mechanical and Aerospace Engineering (SOE)
Language: English
Resource Type: Journal article
Identifiers: 991031666282004646