Author Details
Rui, Zhou
| Issue | Section | Title | File |
| Vol 61, No 5 (2023) | Articles | A Method for Calculating the Trajectory of a Single-Impulse Flight to a Halo Orbit around the L2 Libration Point of the Earth–Moon |
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Keywords
Spacecraft
Sun stabilization
bias current
dissipative forces
drift of magnetic poles
electron concentration
evolution of the rotational motion of the Earth
evolutionary equations
gravitational field
magnetic attitude control
magnetorquers
magnetosphere
photoelectron current density
satellite potential
satellite with a spherical damper (Lavrentiev model)
spherical Langmuir probe
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Pay with
User
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Keywords
Spacecraft
Sun stabilization
bias current
dissipative forces
drift of magnetic poles
electron concentration
evolution of the rotational motion of the Earth
evolutionary equations
gravitational field
magnetic attitude control
magnetorquers
magnetosphere
photoelectron current density
satellite potential
satellite with a spherical damper (Lavrentiev model)
spherical Langmuir probe
Information