Towards a satellite system for archaeology? Simulation of an optical satellite mission with ideal spatial and temporal resolution, illustrated by a case study in Scotland
McGrath, Ciara N. and Scott, Charlie and Cowley, Dave and Macdonald, Malcolm (2020) Towards a satellite system for archaeology? Simulation of an optical satellite mission with ideal spatial and temporal resolution, illustrated by a case study in Scotland. Remote Sensing, 12 (24). 4100. ISSN 2072-4292 (https://doi.org/10.3390/rs12244100)
Preview |
Text.
Filename: McGrath_etal_RS_2020_Towards_a_satellite_system_for_archaeology_simulation_of_an_optical_satellite_mission.pdf
Final Published Version License: Download (2MB)| Preview |
Abstract
Applications of remote sensing data for archaeology rely heavily on repurposed data, which carry inherent limitations in their suitability to help address archaeological questions. Through a case study framed around archaeological imperatives in a Scottish context, this work investigates the potential for existing satellite systems to provide remote sensing data that meet defined specifications for archaeological prospection, considering both spatial and temporal resolution, concluding that the availability of commercial data is currently insufficient. Tasking a commercial constellation of 12 spacecraft to collect images of a 150 km 2 region in Scotland through the month of July 2020 provided 26 images with less than 50% cloud cover. Following an analysis of existing systems, this paper presents a high-level mission architecture for a bespoke satellite system designed from an archaeological specification. This study focuses on orbit design and the number of spacecraft needed to meet the spatial and temporal resolution requirements for archaeological site detection and monitoring in a case study of Scotland, using existing imaging technology. By exploring what an ideal scenario might look like from a satellite mission planning perspective, this paper presents a simulation analysis that foregrounds archaeological imperatives and specifies a satellite constellation design on that basis. High-level design suggests that a system of eight 100 kg spacecraft in a 581 km altitude orbit could provide coverage at a desired temporal and spatial resolution of two-weekly revisit and <1 m ground sampling distance, respectively. The potential for such a system to be more widely applied in regions of similar latitude and climate is discussed.
ORCID iDs
McGrath, Ciara N. ORCID: https://orcid.org/0000-0002-7540-7476, Scott, Charlie, Cowley, Dave and Macdonald, Malcolm ORCID: https://orcid.org/0000-0003-4499-4281;-
-
Item type: Article ID code: 74869 Dates: DateEvent15 December 2020Published11 December 2020Accepted28 August 2020SubmittedSubjects: Technology > Electrical engineering. Electronics Nuclear engineering Department: Faculty of Engineering > Electronic and Electrical Engineering
Technology and Innovation Centre > Advanced Engineering and ManufacturingDepositing user: Pure Administrator Date deposited: 11 Dec 2020 11:56 Last modified: 12 Dec 2024 10:19 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/74869