Spacecraft Relative Motion Applications to Pursuit-Evasion Games and Control Using Angles-Only Navigation
| Metadata Field | Value | Language |
|---|---|---|
| dc.contributor.advisor | Sinclair, Andrew | en_US |
| dc.contributor.author | Jagat, Ashish | en_US |
| dc.date.accessioned | 2015-05-29T13:20:34Z | |
| dc.date.available | 2015-05-29T13:20:34Z | |
| dc.date.issued | 2015-05-29 | |
| dc.identifier.uri | http://hdl.handle.net/10415/4666 | |
| dc.description.abstract | In the first part, applied linear quadratic (LQ) differential game theory to derive linear control laws for orbit pursuit-evasion (PE) problem and extended LQ game theory to nonlinear PE game using the state-dependent Riccati equation (SDRE) method. In the second part, applied linear quadratic dual control method and information-weighted LQG method to improve observability of spacecraft relative motion when angles-only navigation and continuous-thrust maneuvers are used for rendezvous. | en_US |
| dc.subject | Aerospace Engineering | en_US |
| dc.title | Spacecraft Relative Motion Applications to Pursuit-Evasion Games and Control Using Angles-Only Navigation | en_US |
| dc.type | Dissertation | en_US |
| dc.embargo.status | NOT_EMBARGOED | en_US |