The mechanism of grid current dynamic characteristics for microwave discharge ion thruster under the regulation of feedback control system applied in high precision space missions
Author:
Affiliation:
1. Harbin Institute of Technology,School of energy science and engineering,Harbin,China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10625766/10625775/10627204.pdf?arnumber=10627204
Reference5 articles.
1. A minimized electron cyclotron resonance ion thruster for China’s space-borne gravitational wave detection missions
2. Integrative simulation of a 2 cm electron cyclotron resonance ion source with full particle-in-cell method
3. Numerical Simulation of Characteristics of CEX Ions in Ion Thruster Optical System
4. Improving the microwave window breakdown threshold by using a fluorinated, periodically patterned surface
5. Precision Feedback Control Design of Miniature Microwave Discharge Ion Thruster for Space Gravitational Wave Detection
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