Real-Time On-Orbit Estimation Method for Microthruster Thrust Based on High-Precision Orbit Determination
In order to enable the micro-nanosatellites equipped with microthrusters to better complete various space applications, it is necessary to estimate the thrust performance of the microthrusters in real-time on orbit. This paper proposes a real-time on-orbit estimation method for microthrust based on...
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Main Authors: | Qinglin Yang, Weijing Zhou, Hao Chang |
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Format: | Article |
Language: | English |
Published: |
Wiley
2021-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2021/7733495 |
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