Title:
The Improvement of Multi-Satellite Orbit Determination Through the Incorporation of Intersatellite Ranging Observations
The Improvement of Multi-Satellite Orbit Determination Through the Incorporation of Intersatellite Ranging Observations
| dc.contributor.advisor | Gunter, Brian C. | |
| dc.contributor.author | Davis, Byron Taylor | |
| dc.contributor.committeeMember | Lightsey, Edgar G. | |
| dc.contributor.committeeMember | Ho, Koki | |
| dc.contributor.committeeMember | Seubert, Jill | |
| dc.contributor.committeeMember | Gustafson, Eric | |
| dc.contributor.department | Aerospace Engineering | |
| dc.date.accessioned | 2023-01-10T16:20:27Z | |
| dc.date.available | 2023-01-10T16:20:27Z | |
| dc.date.created | 2021-12 | |
| dc.date.issued | 2021-12-14 | |
| dc.date.submitted | December 2021 | |
| dc.date.updated | 2023-01-10T16:20:27Z | |
| dc.description.abstract | For many satellite remote sensing and communications missions, particularly those involving a formation or constellation of satellites, having precise knowledge of the satellites’ positions in both an absolute and relative sense is essential. However, the capabilities of Global Navigation Satellite Systems (GNSS)-based precise orbit determination (POD) alone may not be enough to fulfill the mission’s requirements. This thesis examines potential gains to POD when additional Intersatellite Range (ISR) observations (range magnitude only, not range direction or rate) are combined with standard GNSS observables. These ISR observations can be obtained from simple radio frequency (RF) or optical sensors. The methodology behind the combination approach is described and illustrated through a series of simulated case studies involving multiple satellites in low Earth orbit (LEO) using realistic hardware-derived (where possible) measurement noise. The results demonstrate that substantial improvements (factor of two or better) in the POD of the constellation satellites can be obtained with even intermittent ranging measurements, and with only millimeter-level ranging precision. This improved positioning capability enables new mission concepts for small-satellite constellations and formations, and makes these multi-satellite systems resilient to disruptions in GNSS signal availability. This GNSS-denial could be due to a variety of factors, such as intermittent or total hardware failure, power-related duty cycling, or ground-based jamming. Results show that under appropriate phasing of periodic GNSS-denial, combined with the new information from the ISR observations, POD levels approaching the non-GNSS-denied case can be achieved. For the cases of region-specific or single-satellite total GNSS-denial, constellations with ISR capability can be designed to completely compensate for the loss of GNSS observations and perform at levels better than with GNSS alone. Furthermore, the GNSS-denied case has an extended application for providing ISR-only POD for constellations around planetary bodies through the inversion of the invariant non-spherical gravity fields. Case studies are presented using high resolution invariant Earth and lunar gravity fields. In these example cases, ISR-only POD is demonstrated at the sub-meter level with the same millimeter precision of ISR. This research provides opportunities for new mission concepts that require precise positioning, improvements to mission operations, and enables new paradigms for orbit determination without access to GNSS. | |
| dc.description.degree | Ph.D. | |
| dc.format.mimetype | application/pdf | |
| dc.identifier.uri | http://hdl.handle.net/1853/70079 | |
| dc.language.iso | en_US | |
| dc.publisher | Georgia Institute of Technology | |
| dc.subject | Precise Orbit Determination | |
| dc.subject | GNSS-Denied | |
| dc.subject | Autonomous Lunar Navigation | |
| dc.subject | GNSS Simulation | |
| dc.subject | Intersatellite Ranging | |
| dc.subject | Intersatellite Range Magnitude-Only Precise Orbit Determination | |
| dc.subject | Reduced Dynamics Modelling | |
| dc.subject | Square Root Information Filter | |
| dc.subject | Stochastic Estimation | |
| dc.subject | CubeSat | |
| dc.subject | Constellations | |
| dc.subject | The Ranging and Nanosatellite Guidance Experiment | |
| dc.subject | Chip Scale Atomic Clocks | |
| dc.title | The Improvement of Multi-Satellite Orbit Determination Through the Incorporation of Intersatellite Ranging Observations | |
| dc.type | Text | |
| dc.type.genre | Dissertation | |
| dspace.entity.type | Publication | |
| local.contributor.advisor | Gunter, Brian C. | |
| 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.isAdvisorOfPublication | 76d91d29-f35b-4654-b3d4-2a53708e2c12 | |
| 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 |