Semi-analytical approach for computing near-optimal low-thrust transfers to geosynchronous orbit-Reference-Cited by-同舟云学术

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Semi-analytical approach for computing near-optimal low-thrust transfers to geosynchronous orbit

Published:2016-08 Issue: Volume:55 Page:482-493
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Lei,Xu Bo,Li Muzi,Zhang Fei

Funder

National Basic Research Program 973 of China

Satellite Communication and Navigation Collaborative Innovation Center

Research and Innovation Project for College Graduates of Jiangsu Province

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. Geosynchronous-Earth-orbit communication satellite deliveries with integrated electric propulsion;Byers;J. Propuls. Power,2008

2. Optimum power-limited orbit transfer in strong gravity fields;Edelbaum;AIAA J.,1965

3. Optimal strategy for geostationary orbit acquisition using ion propulsion;Circi;J. Guid. Control Dyn.,2003

4. Solar Electric Geocentric Transfer with Attitude Constraints: Analysis;Sackett,1975

5. Symplectic adaptive algorithm for solving nonlinear two-point boundary value problems in astrodynamics;Peng;Celest. Mech. Dyn. Astron.,2011

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