Displaced Electric Sail Orbits Design and Transition Trajectory Optimization
Displaced orbits for spacecraft propelled by electric sails are investigated as an alternative to the use of solar sails. The orbital dynamics of electric sails based spacecraft are studied within a spherical coordinate system, which permits finding the solutions of displaced electric sail orbits an...
Main Authors: | Naiming Qi, Mingying Huo, Qiufan Yuan |
---|---|
Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2014-01-01
|
Series: | Mathematical Problems in Engineering |
Online Access: | http://dx.doi.org/10.1155/2014/932190 |
Similar Items
-
The Coupled Orbit-Attitude Dynamics and Control of Electric Sail in Displaced Solar Orbits
by: Mingying Huo, et al.
Published: (2017-01-01) -
Coupled attitude-orbit dynamics and control for an electric sail in a heliocentric transfer mission.
by: Mingying Huo, et al.
Published: (2015-01-01) -
Initial Three-Dimensional Trajectory Design for Solar Sails Using Bezier Shaping Approach
by: Mingying Huo, et al.
Published: (2019-01-01) -
Loosely Formation-Displaced Geostationary Orbit Optimization with Complex Hybrid Sail Propulsion
by: Yuan Liu, et al.
Published: (2018-01-01) -
Trajectory design for solar sailing from low-Earth orbit to the Moon
by: Fekete, Thomas A. (Thomas André)
Published: (2007)