A novel model of space electromagnetic docking is established to solve the problem of traditional plume contamination and short service life in this paper. A new modelling technique regarding space electromagnetic docking for CubeSat is proposed. The mathematical model with four core-containing energized solenoids is derived and simplified to the magnetic dipole far-field model of single-turn coil. Simplifying the magnetic dipole far-field model will yield the model of space electromagnetic docking, and the numerical simulation results also verify the reliability and feasibility of simplification process.
Dynamics modeling and simulation of space electromagnetic docking for CubeSat
2017-07-01
451947 byte
Conference paper
Electronic Resource
English
Non-rod-cone type modularized cubesat electromagnetic docking mechanism
European Patent Office | 2024
|CubeSat Autonomous Rendezvous and Docking Software
NTRS | 2015
|Optical design of small space rendezvous and docking lens for CubeSat
British Library Conference Proceedings | 2020
|