Title:
A state machine architecture for aerospace vehicle fault protection
A state machine architecture for aerospace vehicle fault protection
| dc.contributor.author | Schulte, Peter Z. | |
| dc.contributor.committeeMember | Lightsey, Glenn | |
| dc.contributor.committeeMember | Costello, Mark F. | |
| dc.contributor.committeeMember | Smith, Neil G. | |
| dc.contributor.committeeMember | Rosendall, Paul | |
| dc.contributor.department | Aerospace Engineering | |
| dc.date.accessioned | 2018-08-20T15:36:22Z | |
| dc.date.available | 2018-08-20T15:36:22Z | |
| dc.date.created | 2018-08 | |
| dc.date.issued | 2018-06-13 | |
| dc.date.submitted | August 2018 | |
| dc.date.updated | 2018-08-20T15:36:22Z | |
| dc.description.abstract | Because of their complexity and the unforgiving environment in which they operate, aerospace vehicles are vulnerable to mission-critical failures. In order to prevent these failures, aerospace vehicles often employ Fault Detection, Isolation, and Recovery (FDIR) systems to sense, identify the source of, and recover from faults. Typically, aerospace systems use a rule-based paradigm for FDIR where telemetry values are monitored against specific logical statements such as static upper and lower limits. The model-based paradigm allows more complex decision logic to be used for FDIR. State machines are a particular tool for model-based FDIR that have been explored by industry but not yet widely adopted. This study develops a generic and modular state machine FDIR architecture that is portable to flight software. The study will focus on FDIR for the Guidance, Navigation, & Control subsystem, but it will be presented in a manner that is applicable to all vehicle subsystems. The state machine formulation is applied for on-board model-based fault diagnosis. Two specific case studies are employed to demonstrate the architecture. The first is a terrestrial application of unmanned aerial vehicles for 3D scanning and mapping, which is validated through flight testing. The second is a space-based application of automated close approach and capture for a Mars sample return mission, which is validated through software-in-the-loop testing with flight-like software components. | |
| dc.description.degree | Ph.D. | |
| dc.format.mimetype | application/pdf | |
| dc.identifier.uri | http://hdl.handle.net/1853/60252 | |
| dc.language.iso | en_US | |
| dc.publisher | Georgia Institute of Technology | |
| dc.subject | Fault protection | |
| dc.subject | Fault detection, isolation, and recovery | |
| dc.subject | Guidance, navigation, and control | |
| dc.subject | State machines | |
| dc.subject | On-board fault diagnosis | |
| dc.subject | Aerospace systems engineering | |
| dc.title | A state machine architecture for aerospace vehicle fault protection | |
| dc.type | Text | |
| dc.type.genre | Dissertation | |
| dspace.entity.type | Publication | |
| local.contributor.corporatename | College of Engineering | |
| local.contributor.corporatename | Daniel Guggenheim School of Aerospace Engineering | |
| local.relation.ispartofseries | Doctor of Philosophy with a Major in Aerospace Engineering | |
| relation.isOrgUnitOfPublication | 7c022d60-21d5-497c-b552-95e489a06569 | |
| relation.isOrgUnitOfPublication | a348b767-ea7e-4789-af1f-1f1d5925fb65 | |
| relation.isSeriesOfPublication | f6a932db-1cde-43b5-bcab-bf573da55ed6 | |
| thesis.degree.level | Doctoral |