Hybrid Low Thrust Propulsion Trajectory Design and Optimization Using Virtual Gravity Method
a novel spacecraft trajectory design method using hybrid low thrust system is proposed in this paper. The hybrid system is constituted with a solar sail propulsion thruster and a solar electric propulsion thruster. In proposed method, the former one provides radical thrust and circumferential thrust...
Format: | Article |
---|---|
Language: | zho |
Published: |
EDP Sciences
2018-08-01
|
Series: | Xibei Gongye Daxue Xuebao |
Subjects: | |
Online Access: | https://www.jnwpu.org/articles/jnwpu/pdf/2018/04/jnwpu2018364p618.pdf |
Similar Items
-
A New 3D Shaping Method for Low-Thrust Trajectories between Non-Intersect Orbits
by: Tongxin Zhang, et al.
Published: (2021-10-01) -
Lifetime Extension of Ultra Low-Altitude Lunar Spacecraft with Low-Thrust Propulsion System
by: Jingxi Liu, et al.
Published: (2022-06-01) -
A design of wind powered propulsion system /
by: 294695 Shahrizwan Effendi Hashmi
Published: (2005) -
A design of wind powered propulsion system [compact disc] /
by: 294695 Shahrizwan Effendi Hashmi
Published: (2006) -
Initial Costate Approximation for Rapid Orbit Raising with Very Low Propulsive Acceleration
by: Alessandro A. Quarta
Published: (2024-01-01)