Automated near real-time validation and exploitation of optical sensor data for improved orbital safety. (April 2019)
- Record Type:
- Journal Article
- Title:
- Automated near real-time validation and exploitation of optical sensor data for improved orbital safety. (April 2019)
- Main Title:
- Automated near real-time validation and exploitation of optical sensor data for improved orbital safety
- Authors:
- Kelecy, Thomas
Lambert, Emily
Sunderland, Benjamin
Stauch, Jason
Mallik, Vishnuu
Jah, Moriba - Abstract:
- Abstract: The orbital safety of operational spacecraft, regardless of the mission, relies on timely and actionable observations to maintain so-called "custody" of all trackable Resident Space Objects (RSOs), including space debris, that might pose a hazard to safe, secure, and sustainable operations. For operations in and around the Geosynchronous Earth Orbit (GEO) regime, electro-optical (EO) observations are the most prevalent observation type available for tracking and determining RSO orbits. The quality (both accuracy and precision) of the data affects the inferable kinematic, physical, and other characteristics of RSOs and, in particular, measurement biases will result in inaccurate orbital trajectories and subsequent predictions. Physically meaningful conjunction assessments rely on not only accurate orbit state prediction, but also the "realistic" covariances associated with said predictions. In this paper we demonstrate an automated near real-time (NRT) assessment of measurement biases with an appropriately implemented Unscented Schmidt Kalman Filter (USKF) [14]. Hypothesized biases that are deterministic but statistically unobservable in the measurement data and cannot be estimated are accounted for as so-called "consider" parameters. The method presented herein is assessed and quantified using both simulated and actual measurement data. This method will enable the exploitation and mining of so-called "non-traditional" sensor data to maximize Space SituationalAbstract: The orbital safety of operational spacecraft, regardless of the mission, relies on timely and actionable observations to maintain so-called "custody" of all trackable Resident Space Objects (RSOs), including space debris, that might pose a hazard to safe, secure, and sustainable operations. For operations in and around the Geosynchronous Earth Orbit (GEO) regime, electro-optical (EO) observations are the most prevalent observation type available for tracking and determining RSO orbits. The quality (both accuracy and precision) of the data affects the inferable kinematic, physical, and other characteristics of RSOs and, in particular, measurement biases will result in inaccurate orbital trajectories and subsequent predictions. Physically meaningful conjunction assessments rely on not only accurate orbit state prediction, but also the "realistic" covariances associated with said predictions. In this paper we demonstrate an automated near real-time (NRT) assessment of measurement biases with an appropriately implemented Unscented Schmidt Kalman Filter (USKF) [14]. Hypothesized biases that are deterministic but statistically unobservable in the measurement data and cannot be estimated are accounted for as so-called "consider" parameters. The method presented herein is assessed and quantified using both simulated and actual measurement data. This method will enable the exploitation and mining of so-called "non-traditional" sensor data to maximize Space Situational Awareness (SSA) in a robust and timely fashion toward improvement of orbital safety. The ultimate goal is to provide decision-making evidence required solve problems preventing the space domain from being safe, secure, and sustainable. Highlights: Addresses need to supplement surveillance networks with "non-traditional" data. Goal of work is to characterize data integrity in near real-time. Collaboration funded by European Office of Aerospace Research and Development. Dynamic "multi-state" filter estimates sensor noise and bias characteristics. Combined state estimation uses consider covariance to determine error sensitivity. … (more)
- Is Part Of:
- Acta astronautica. Volume 157(2019)
- Journal:
- Acta astronautica
- Issue:
- Volume 157(2019)
- Issue Display:
- Volume 157, Issue 2019 (2019)
- Year:
- 2019
- Volume:
- 157
- Issue:
- 2019
- Issue Sort Value:
- 2019-0157-2019-0000
- Page Start:
- 404
- Page End:
- 414
- Publication Date:
- 2019-04
- Subjects:
- Estimation -- Dynamic sensor calibration -- Orbital safety
Astronautics -- Periodicals
Outer space -- Exploration -- Periodicals
Astronautics
Periodicals
629.405 - Journal URLs:
- http://www.sciencedirect.com/science/journal/00945765 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.actaastro.2018.12.043 ↗
- Languages:
- English
- ISSNs:
- 0094-5765
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 0596.750000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 9622.xml