Abstract
An optimal control scheme for attitude control of rigid body spacecraft is proposed in this paper. The dynamic optimal control problem is first converted into a nonlinear programming problem (NLP) by Legendre pseudospectral method (LPM) and then this NLP problem is solved. The time as well as energy is optimized for the rigid body spacecraft using LPM. The re-orientation problem of the rigid spacecraft is solved both as a regulation problem and then as a tracking problem. The simulation is carried out using a Matlabc toolbox called DIDO and the simulation results illustrates the desired performances of spacecraft attitude regulation and tracking.
| Original language | English |
|---|---|
| Title of host publication | 2019 5th Indian Control Conference, ICC 2019 - Proceedings |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 347-352 |
| Number of pages | 6 |
| ISBN (Electronic) | 9781538662465 |
| DOIs | |
| State | Published - 14 May 2019 |
| Externally published | Yes |
| Event | 5th Indian Control Conference, ICC 2019 - Delhi, India Duration: 9 Jan 2019 → 11 Jan 2019 |
Publication series
| Name | 2019 5th Indian Control Conference, ICC 2019 - Proceedings |
|---|
Conference
| Conference | 5th Indian Control Conference, ICC 2019 |
|---|---|
| Country/Territory | India |
| City | Delhi |
| Period | 9/01/19 → 11/01/19 |
Bibliographical note
Publisher Copyright:© 2019 IEEE.
ASJC Scopus subject areas
- Control and Systems Engineering
- Control and Optimization