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Average Cross-Sectional Area of DebriSat Fragments Using Volumetrically Constructed 3D RepresentationsDebris fragments from the hypervelocity impact testing of DebriSat are being collected and characterized for use in updating existing satellite breakup models. One of the key parameters utilized in these models is the ballistic coefficient of the fragment which is directly related to its area‐to‐mass ratio. However, since the attitude of fragments varies during their orbital lifetime, it is customary to use the average cross‐sectional area in the calculation of the area‐to‐mass ratio. The average cross‐sectional area is defined as the average of the projected surface areas perpendicular to the direction of motion and has been shown to be equal to one‐fourth of the total surface area of a convex object. Unfortunately, numerous fragments obtained from the DebriSat experiment show significant concavity (i.e., shadowing) and thus we have explored alternate methods for computing the average cross‐sectional area of the fragments. An imaging system based on the volumetric reconstruction of a 3D object from multiple 2D photographs of the object was developed for use in determining the size characteristic (i.e., characteristics length) of the DebriSat fragments. For each fragment, the imaging system generates N number of images from varied azimuth and elevation angles and processes them using a space‐carving algorithm to construct a 3D point cloud of the fragment. This paper describes two approaches for calculating the average cross‐sectional area of debris fragments based on the 3D imager. Approach A utilizes the constructed 3D object to generate equally distributed cross‐sectional area projections and then averages them to determine the average cross‐sectional area. Approach B utilizes a weighted average of the area of the 2D photographs to directly compute the average cross‐sectional area. A comparison of the accuracy and computational needs of each approach is described as well as preliminary results of an analysis to determine the "optimal" number of images needed for the 3D imager to accurately measure the average cross sectional area of objects with known dimensions.
Document ID
20160003482
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Scruggs, T.
(Florida Univ. Gainesville, FL, United States)
Moraguez, M.
(Florida Univ. Gainesville, FL, United States)
Patankar, K.
(Florida Univ. Gainesville, FL, United States)
Fitz-Coy, N.
(Florida Univ. Gainesville, FL, United States)
Liou, J.-C.
(NASA Johnson Space Center Houston, TX, United States)
Sorge, M.
(Aerospace Corp. El Segundo, CA, United States)
Huynh, T.
(Air Force Space Command, Space and Missile Systems Center (SMC) Los Angeles AFB, CA, United States)
Date Acquired
March 16, 2016
Publication Date
September 26, 2016
Subject Category
Instrumentation And Photography
Report/Patent Number
JSC-CN-35704
Report Number: JSC-CN-35704
Meeting Information
Meeting: International Astronautical Congress
Location: Guadalajara
Country: Mexico
Start Date: September 26, 2016
End Date: September 30, 2016
Sponsors: International Inst. of Space Law (IISL), Secretaria de Comunicaciones y Transportes, International Astronautical Federation, International Academy of Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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