Abstract
The regulation of satellite orientation in an orbit is an essential task for the success of a space mission. To reorient the attitude of a satellite from an initial point to the desired attitude, efficient control law needs to be developed. In this paper, the attitude control law is proposed to achieve a necessary shortest path of the Eigen-axis rotation between two attitudes. Moreover, it is also shown that the optimization of input energy required for the optimal Eigen-axis rotation can also be done through the proposed approach. The stability analysis of the proposed methodology is proved using the Lyapunov theory. Furthermore, the proposed scheme is also validated through numerical simulation.
| Original language | English |
|---|---|
| Title of host publication | 2020 International Conference on Decision Aid Sciences and Application, DASA 2020 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 783-787 |
| Number of pages | 5 |
| ISBN (Electronic) | 9781728196770 |
| DOIs | |
| State | Published - 8 Nov 2020 |
| Externally published | Yes |
Publication series
| Name | 2020 International Conference on Decision Aid Sciences and Application, DASA 2020 |
|---|
Bibliographical note
Publisher Copyright:© 2020 IEEE.
Keywords
- Attitude Stabilization
- Eigen-axis Rotation
- Lyapunov Theory
- Regulation Control
- Rigid Spacecraft
ASJC Scopus subject areas
- Artificial Intelligence
- Computer Science Applications
- Decision Sciences (miscellaneous)
- Information Systems and Management
- Control and Optimization
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