Introducing the nonlinear state control algorithm of the air bearing laboratory simulator based on the gain coefficients dependent on the state variables
In this article, a new approach has been presented in the design of a satellite's status controller using reaction wheels. First, a non-linear controller whose gains depend on the state variables at any moment is proposed. In the first step, the process of extracting control coefficients using...
Main Authors: | Alireza Ahangarani Farahani, Amirhossain Adami, Hamed Arefkhani |
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Format: | Article |
Language: | fas |
Published: |
Aerospace Research Institute
2023-09-01
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Series: | فصلنامه علوم و فناوری فضایی |
Subjects: | |
Online Access: | https://jsst.ias.ir/article_176258_d615c7c473dc24aa6e44bba5909bc360.pdf |
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