Prediction of hypervelocity orbital debris impact damage to the space station by neural networks
Prediction of damage to orbiting space craft due to collisions with hypervelocity space debris is an important issue in the design of Space Station Freedom. Space station wall structures are designed to absorb impact energy during a collision. A proposed wall structure consists of a multilayer insul...
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| Vydáno v: | Mathematical and computer modelling Ročník 21; číslo 1; s. 229 - 242 |
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| Hlavní autoři: | , |
| Médium: | Journal Article |
| Jazyk: | angličtina |
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Elsevier Ltd
1995
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| ISSN: | 0895-7177, 1872-9479 |
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| Abstract | Prediction of damage to orbiting space craft due to collisions with hypervelocity space debris is an important issue in the design of Space Station
Freedom. Space station wall structures are designed to absorb impact energy during a collision. A proposed wall structure consists of a multilayer insulation (MLI) directly covering the pressure wall, and a bumper layer placed 100mm from the pressure wall. In experiments at The Marshall Space Flight Center, 2.5–12.7 mm projectiles have been fired at this wall structure at speeds of 2–8 km/s. In this paper, three-layer backpropagation networks are trained with two sets of impact damage data. The input parameters for training are pressure wall thickness, bumper plate thickness, projectile diameter, impact angle, and the projectile velocity. Output from the network consists of hole dimensions for the bumper and the pressure wall in the minor and major axis directions, and damage to the MLI. To evaluate network generalization, networks are tested with experimental data points that are not used for training. Network performance is compared with that of other damage prediction methods. Network determination of qualitative damage estimation is suggested as a new direction for research. Preliminary testing of qualitative prediction of pressure wall damage is presented. The results are promising, and suggest several areas for further study. |
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| AbstractList | Prediction of damage to orbiting space craft due to collisions with hypervelocity space debris is an important issue in the design of Space Station
Freedom. Space station wall structures are designed to absorb impact energy during a collision. A proposed wall structure consists of a multilayer insulation (MLI) directly covering the pressure wall, and a bumper layer placed 100mm from the pressure wall. In experiments at The Marshall Space Flight Center, 2.5–12.7 mm projectiles have been fired at this wall structure at speeds of 2–8 km/s. In this paper, three-layer backpropagation networks are trained with two sets of impact damage data. The input parameters for training are pressure wall thickness, bumper plate thickness, projectile diameter, impact angle, and the projectile velocity. Output from the network consists of hole dimensions for the bumper and the pressure wall in the minor and major axis directions, and damage to the MLI. To evaluate network generalization, networks are tested with experimental data points that are not used for training. Network performance is compared with that of other damage prediction methods. Network determination of qualitative damage estimation is suggested as a new direction for research. Preliminary testing of qualitative prediction of pressure wall damage is presented. The results are promising, and suggest several areas for further study. |
| Author | Guleyupoglu, S. Smith, R.E. |
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| Cites_doi | 10.2514/3.11517 10.1086/106009 |
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| Keywords | Nonlinear system modeling Backpropagation learning algorithm Neural network applications Aerospace Damage estimation |
| Language | English |
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| References | Hecht-Nielson (BIB3) 1991 Petro, Ashley (BIB5) 1989; Vol. 121 Hines, Montgomery (BIB14) 1980 McCormick (BIB6) 1989; Vol. 121 Schonberg, Bean, Darzi (BIB1) 1990 Rule (BIB10) September/October 1992; 29 Miyata (BIB13) 1990 Rule, Hayashida (BIB2) 1991 Petro, Talent (BIB4) 1989; Vol. 121 Whipple (BIB8) 1947 Coronado, Gibbins, Wright, Stern (BIB9) 1987 Rumelhart, McClelland (BIB12) 1986; Vol. 1 Kline, McCaffrey, Stein (BIB7) 1985; Vol. 99 Taylor (BIB11) February 1987; 18 Schonberg (10.1016/0895-7177(94)00206-4_BIB1) 1990 Miyata (10.1016/0895-7177(94)00206-4_BIB13) 1990 Rule (10.1016/0895-7177(94)00206-4_BIB10) 1992; 29 Rule (10.1016/0895-7177(94)00206-4_BIB2) 1991 Whipple (10.1016/0895-7177(94)00206-4_BIB8) 1947 Coronado (10.1016/0895-7177(94)00206-4_BIB9) 1987 Taylor (10.1016/0895-7177(94)00206-4_BIB11) 1987; 18 Kline (10.1016/0895-7177(94)00206-4_BIB7) 1985; Vol. 99 Hines (10.1016/0895-7177(94)00206-4_BIB14) 1980 Petro (10.1016/0895-7177(94)00206-4_BIB5) 1989; Vol. 121 McCormick (10.1016/0895-7177(94)00206-4_BIB6) 1989; Vol. 121 Rumelhart (10.1016/0895-7177(94)00206-4_BIB12) 1986; Vol. 1 Hecht-Nielson (10.1016/0895-7177(94)00206-4_BIB3) 1991 Petro (10.1016/0895-7177(94)00206-4_BIB4) 1989; Vol. 121 |
| References_xml | – start-page: 131 year: 1947 ident: BIB8 article-title: Meteorites and space travel publication-title: Astronomical Journal – year: 1990 ident: BIB1 article-title: Hypervelocity impact physics publication-title: NASA Contractor Report 4343 – year: 1991 ident: BIB3 article-title: Neurocomputing – volume: Vol. 121 start-page: 183 year: 1989 end-page: 186 ident: BIB5 article-title: Cost estimates for removal of orbital debris publication-title: Orbital Debris from Upper Stage Breakup – volume: Vol. 99 start-page: 290 year: 1985 ident: BIB7 article-title: A summary of potential designs of space stations and platforms publication-title: Space Stations and Space Platforms—Concepts, Design, Infrastructure, and Uses – volume: Vol. 121 start-page: 169 year: 1989 end-page: 182 ident: BIB4 article-title: Removal of orbital debris publication-title: Orbital Debris from Upper Stage Breakup – volume: Vol. 121 start-page: 187 year: 1989 end-page: 197 ident: BIB6 article-title: Collision probabilities in geosynchronous orbit and techniques to control the environment publication-title: Orbital Debris from Upper Stage Breakup – volume: 29 start-page: 727 year: September/October 1992 end-page: 734 ident: BIB10 article-title: Testing and numerical modeling of hypervelocity impact damaged Space Station multilayer insulation publication-title: Journal of Spacecraft and Rockets – volume: 18 start-page: 28 year: February 1987 end-page: 34 ident: BIB11 article-title: A space debris simulation facility for spacecraft materials evaluation publication-title: SAMPE Quarterly – year: 1991 ident: BIB2 article-title: Empirical predictions of hypervelocity impact damage to the space station publication-title: NASA Technical Memorandum TM-103550 – volume: Vol. 1 year: 1986 ident: BIB12 publication-title: Parallel Distributed Processing: Explorations in the Microstructure of Cognition – year: 1990 ident: BIB13 publication-title: A user's guide to Planet Version 5.6 – year: 1980 ident: BIB14 article-title: Probability and Statistics in Engineering and Management Science – year: 1987 ident: BIB9 article-title: Space station integrated wall design and penetration damage control publication-title: D 180-30550-1 – volume: 29 start-page: 727 issue: 5 year: 1992 ident: 10.1016/0895-7177(94)00206-4_BIB10 article-title: Testing and numerical modeling of hypervelocity impact damaged Space Station multilayer insulation publication-title: Journal of Spacecraft and Rockets doi: 10.2514/3.11517 – year: 1980 ident: 10.1016/0895-7177(94)00206-4_BIB14 – volume: Vol. 121 start-page: 187 year: 1989 ident: 10.1016/0895-7177(94)00206-4_BIB6 article-title: Collision probabilities in geosynchronous orbit and techniques to control the environment – volume: Vol. 99 start-page: 290 year: 1985 ident: 10.1016/0895-7177(94)00206-4_BIB7 article-title: A summary of potential designs of space stations and platforms – year: 1987 ident: 10.1016/0895-7177(94)00206-4_BIB9 article-title: Space station integrated wall design and penetration damage control – volume: Vol. 121 start-page: 169 year: 1989 ident: 10.1016/0895-7177(94)00206-4_BIB4 article-title: Removal of orbital debris – volume: Vol. 121 start-page: 183 year: 1989 ident: 10.1016/0895-7177(94)00206-4_BIB5 article-title: Cost estimates for removal of orbital debris – start-page: 131 issue: 1161 year: 1947 ident: 10.1016/0895-7177(94)00206-4_BIB8 article-title: Meteorites and space travel publication-title: Astronomical Journal doi: 10.1086/106009 – volume: 18 start-page: 28 year: 1987 ident: 10.1016/0895-7177(94)00206-4_BIB11 article-title: A space debris simulation facility for spacecraft materials evaluation publication-title: SAMPE Quarterly – year: 1990 ident: 10.1016/0895-7177(94)00206-4_BIB13 publication-title: A user's guide to Planet Version 5.6 – volume: Vol. 1 year: 1986 ident: 10.1016/0895-7177(94)00206-4_BIB12 – year: 1991 ident: 10.1016/0895-7177(94)00206-4_BIB3 – year: 1990 ident: 10.1016/0895-7177(94)00206-4_BIB1 article-title: Hypervelocity impact physics – year: 1991 ident: 10.1016/0895-7177(94)00206-4_BIB2 article-title: Empirical predictions of hypervelocity impact damage to the space station |
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Freedom.... |
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| SubjectTerms | Aerospace Backpropagation learning algorithm Damage estimation Neural network applications Nonlinear system modeling |
| Title | Prediction of hypervelocity orbital debris impact damage to the space station by neural networks |
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