TY - JOUR
T1 - Reconstruction of Bennu Particle Events From Sparse Data
AU - Pelgrift, John Y.
AU - Lessac-Chenen, Erik J.
AU - Adam, Coralie D.
AU - Leonard, Jason M.
AU - Nelson, Derek S.
AU - McCarthy, Leilah
AU - Sahr, Eric M.
AU - Liounis, Andrew
AU - Moreau, Michael
AU - Bos, Brent J.
AU - Hergenrother, Carl W.
AU - Lauretta, Dante S.
N1 - Funding Information:
We are grateful to the entire OSIRIS‐REx Team for making the encounter with Bennu possible. This material is based upon work supported by the National Aeronautics and Space Administration under Contracts NG13FC02C and NNM10AA11C issued through the New Frontiers Program. NavCam 1 images are available in the TAGCAMS data bundle via the Planetary Data System (PDS) (Bos et al., ). Data are delivered to the PDS according to the OSIRIS‐REx Data Management Plan available in the OSIRIS‐REx PDS archive (Crombie & Selznick, ). The data used to generate the figures in this paper are available via Figshare data repository (Pelgrift et al., ). The software used in this analysis is proprietary to KinetX, Inc.; however, section shows how the relevant information was extracted from the image data set.
Publisher Copyright:
©2020. The Authors.
PY - 2020/8/1
Y1 - 2020/8/1
N2 - OSIRIS-REx began observing particle ejection events shortly after entering orbit around near-Earth asteroid (101955) Bennu in January 2019. For some of these events, the only observations of the ejected particles come from the first two images taken immediately after the event by OSIRIS-REx's NavCam 1 imager. Without three or more observations of each particle, traditional orbit determination is not possible. However, by assuming that the particles all ejected at the same time and location for a given event, and approximating that their velocities remained constant after ejection (a reasonable approximation for fast-moving particles, i.e., with velocities on the order of 10 cm/s or greater, given Bennu's weak gravity), we show that it is possible to estimate the particles' states from only two observations each. We applied this newly developed technique to reconstruct the particle ejection events observed by the OSIRIS-REx spacecraft during orbit about Bennu. Particles were estimated to have ejected with inertial velocities ranging from 7 cm/s to 3.3 m/s, leading to a variety of trajectory types. Most (>80%) of the analyzed events were estimated to have originated from midlatitude regions and to have occurred after noon (local solar time), between 12:44 and 18:52. Comparison with higher-fidelity orbit determination solutions for the events with sufficient observations demonstrates the validity of our approach and also sheds light on its biases. Our technique offers the capacity to meaningfully constrain the properties of particle ejection events from limited data.
AB - OSIRIS-REx began observing particle ejection events shortly after entering orbit around near-Earth asteroid (101955) Bennu in January 2019. For some of these events, the only observations of the ejected particles come from the first two images taken immediately after the event by OSIRIS-REx's NavCam 1 imager. Without three or more observations of each particle, traditional orbit determination is not possible. However, by assuming that the particles all ejected at the same time and location for a given event, and approximating that their velocities remained constant after ejection (a reasonable approximation for fast-moving particles, i.e., with velocities on the order of 10 cm/s or greater, given Bennu's weak gravity), we show that it is possible to estimate the particles' states from only two observations each. We applied this newly developed technique to reconstruct the particle ejection events observed by the OSIRIS-REx spacecraft during orbit about Bennu. Particles were estimated to have ejected with inertial velocities ranging from 7 cm/s to 3.3 m/s, leading to a variety of trajectory types. Most (>80%) of the analyzed events were estimated to have originated from midlatitude regions and to have occurred after noon (local solar time), between 12:44 and 18:52. Comparison with higher-fidelity orbit determination solutions for the events with sufficient observations demonstrates the validity of our approach and also sheds light on its biases. Our technique offers the capacity to meaningfully constrain the properties of particle ejection events from limited data.
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U2 - 10.1029/2019EA000938
DO - 10.1029/2019EA000938
M3 - Article
AN - SCOPUS:85089831508
SN - 2333-5084
VL - 7
JO - Earth and Space Science
JF - Earth and Space Science
IS - 8
M1 - e2019EA000938
ER -