Hybrid propulsion spacecraft formation control around the planetary displaced orbit-Reference-Cited by-同舟云学术

Hybrid propulsion spacecraft formation control around the planetary displaced orbit

Published:2021-10 Issue:10 Volume:13 Page:168781402110514
ISSN:1687-8140
Container-title:Advances in Mechanical Engineering
language:en
Short-container-title:Advances in Mechanical Engineering

Author:

Zhao Lei¹^ORCID,Yuan Changqing²,Hao Qingbo¹,He Jingjiu¹

Affiliation:

1. School of Aviation Operations and Services, Air Force Aviation University, Changchun, China

2. Basic Sciences Department, Air Force Aviation University, Changchun, China

Abstract

This paper aims to investigate the feasibility of using the combination of solar radiation pressure and Coulomb force as a propellantless control method for spacecraft formation around the planetary displaced orbit. Firstly, the dynamical equation of spacecraft formation is derived and linearized. Based on the linearized dynamic model, an integral sliding mode controller (ISMC) is designed. Aimed to stabilize the spacecraft formation, the control method is proposed to adjust the product of the charge and the attitude angles of two spacecrafts. Finally, numerical simulations are conducted and the results show that the controller can make the formation achieve the desired configuration with favorable control performances.

Funder

National Natural Science Foundation of China

Publisher

SAGE Publications

Subject

Mechanical Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/16878140211051454

Reference24 articles.

1. King LB, Parker GG, Deshmukh S, et al. Spacecraft formation flying using inter-vehicle coulomb force. Technical Report NASA/NIAC, Michigan Technological University, USA, January 2002.

2. New families of Sun-centered non-Keplerian orbits over cylinders and spheres

3. Solar Sailing

4. Interplanetary trajectory design for a hybrid propulsion system

5. Tradeoff Performance of Hybrid Low-Thrust Propulsion System

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Optimal hybrid Coulomb control for on-track rendezvous and docking of spacecraft;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-03-22

2. Dynamics, Stability, and Cooperative Formation Control of Magnetic Sail-Based Planetary Displaced Orbits;International Journal of Aeronautical and Space Sciences;2022-10-18

3. Magneto plasma sail formation reconfiguration around a heliocentric elliptic displaced orbit;Astrophysics and Space Science;2022-08

4. Multiple Spacecraft Formation Flying Control around Artificial Equilibrium Point Using Propellantless Approach;International Journal of Aerospace Engineering;2022-05-02