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...

Full description

Bibliographic Details
Main Authors: Alireza Ahangarani Farahani, Amirhossain Adami, Hamed Arefkhani
Format: Article
Language:fas
Published: Aerospace Research Institute 2023-09-01
Series:فصلنامه علوم و فناوری فضایی
Subjects:
Online Access:https://jsst.ias.ir/article_176258_d615c7c473dc24aa6e44bba5909bc360.pdf