Design and testing of magnetic controllers for Satellite stabilization-Reference-Cited by-同舟云学术

Design and testing of magnetic controllers for Satellite stabilization

Published:2005-01 Issue:1-2 Volume:56 Page:231-239
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Guelman M.,Waller R.,Shiryaev A.,Psiaki M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference5 articles.

1. The TechSAT-1 attitude estimation by telemetry processing;Karmanov,1999

2. Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation;Psiaki;Journal of Guidance Control and Dynamics,2001

3. A globally stable linear attitude regulator;Mortensen;International Journal of Control,1968

4. M. Shachar, Private communication.

5. G. Shaviv, M. Shachar, Techsat-1—an Earth-pointing 3-axis stabilized microsatellite, in: Proceedings of the 45th Congress of the International Astronautical Federation, October 1994, Jerusalem, Israel, paper IAA 94-IAA.11.2.767.

Cited by 31 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Monoaxial Electrodynamic Stabilization of a Spacecraft Using PID Controller;Mekhatronika, Avtomatizatsiya, Upravlenie;2024-07-18

2. Triaxial electrodynamic stabilization of a satellite via PID controller;Vestnik of Saint Petersburg University. Applied Mathematics. Computer Science. Control Processes;2024

3. Calibration of Onboard Magnetometers of the Attitude Control System of the SamSat-ION University Nanosatellite;Gyroscopy and Navigation;2023-09

4. Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame;Aerospace Science and Technology;2022-08

5. Attitude determination and control for the deployment preparation phase of a space tether mission;Acta Astronautica;2022-04