Abstract
This article investigates the order-reduction method for multi-spacecraft cooperative tracking control problems considering non-uniform time delays. The tracking error system is constructed as a linear time-varying (LTV) system since the orbit of the reference point is an ellipse. To facilitate the controller design, a model transformation method is proposed to transform the LTV system into a linear time-invariant (LTI) system with norm-bounded uncertainties. By using the sliding-mode control (SMC) technique, a delay-dependent cooperative tracking controller is designed to guarantee multiple followers to track the leader. Then, an order-reduction method is proposed to reduce the order of sufficient conditions in the form of linear matrix inequalities (LMIs), which make sure that the tracking error system is asymptotically stable. A numerical example is finally provided to illustrate the effectiveness of the designed controller and the improved performance of the order-reduction method.
| Original language | English |
|---|---|
| Pages (from-to) | 2849-2873 |
| Number of pages | 25 |
| Journal | Journal of the Franklin Institute |
| Volume | 355 |
| Issue number | 5 |
| DOIs | |
| State | Published - Mar 2018 |
Fingerprint
Dive into the research topics of 'Improved order-reduction method for cooperative tracking control of time-delayed multi-spacecraft network'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver