Flight mechanics/Navigation/Control/...
Automatic Mass Balancing of Spacecraft Attitude Simulator by Parameter Estimation and Linear Control

M. Barati; Mehdi Sabzehparvar; M. Navabi

Volume 8, Issue 2 , June 2024, , Pages 55-65

https://doi.org/10.22034/jtae.2024.8.2.5

Abstract
  In order to perform attitude control ground experiments, it is crucial to ensure the center of mass of the platform is coincident with the center of rotation as accurate as possible. In this paper, a linearized dynamic model of the imbalanced attitude platform is derived and a linear controller is methodically ...  Read More