36 results on '"ground target"'
Search Results
2. 地面目标HRRP识别的稳健性特征选择方法.
- Author
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刘丹阳, 吴堃, 朱永锋, 张永杰, and 周剑雄
- Subjects
RADAR targets ,FEATURE selection ,FEATURE extraction - Abstract
Copyright of Systems Engineering & Electronics is the property of Journal of Systems Engineering & Electronics Editorial Department and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
- Published
- 2023
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- View/download PDF
3. Development of Ground Target Image Recognition System Based on Deep Learning Technology
- Author
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Jiang, Rui, Jiang, Yuan, Chen, Qiaoling, Xhafa, Fatos, Series Editor, Xu, Zheng, editor, Alrabaee, Saed, editor, Loyola-González, Octavio, editor, Cahyani, Niken Dwi Wahyu, editor, and Ab Rahman, Nurul Hidayah, editor
- Published
- 2023
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- View/download PDF
4. Image-Based Sliding Mode Attitude Control Research on Small Video Satellites
- Author
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Wang, Mengmeng, Song, Chao, Fan, Caizhi, Zhang, Yonghe, Angrisani, Leopoldo, Series Editor, Arteaga, Marco, Series Editor, Panigrahi, Bijaya Ketan, Series Editor, Chakraborty, Samarjit, Series Editor, Chen, Jiming, Series Editor, Chen, Shanben, Series Editor, Chen, Tan Kay, Series Editor, Dillmann, Rüdiger, Series Editor, Duan, Haibin, Series Editor, Ferrari, Gianluigi, Series Editor, Ferre, Manuel, Series Editor, Hirche, Sandra, Series Editor, Jabbari, Faryar, Series Editor, Jia, Limin, Series Editor, Kacprzyk, Janusz, Series Editor, Khamis, Alaa, Series Editor, Kroeger, Torsten, Series Editor, Li, Yong, Series Editor, Liang, Qilian, Series Editor, Martín, Ferran, Series Editor, Ming, Tan Cher, Series Editor, Minker, Wolfgang, Series Editor, Misra, Pradeep, Series Editor, Möller, Sebastian, Series Editor, Mukhopadhyay, Subhas, Series Editor, Ning, Cun-Zheng, Series Editor, Nishida, Toyoaki, Series Editor, Oneto, Luca, Series Editor, Pascucci, Federica, Series Editor, Qin, Yong, Series Editor, Seng, Gan Woon, Series Editor, Speidel, Joachim, Series Editor, Veiga, Germano, Series Editor, Wu, Haitao, Series Editor, Zamboni, Walter, Series Editor, Zhang, Junjie James, Series Editor, Wang, Liheng, editor, Wu, Yirong, editor, and Gong, Jianya, editor
- Published
- 2023
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5. Review of Dynamic Task Allocation Methods for UAV Swarms Oriented to Ground Targets
- Author
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Qiang Peng, Husheng Wu, and Ruisong Xue
- Subjects
unmanned aerial vehicle swarm ,ground target ,dynamic ,task allocation ,research status ,Electronic computers. Computer science ,QA75.5-76.95 ,Systems engineering ,TA168 - Abstract
Dynamic task allocation of unmanned aerial vehicle swarms for ground targets is an important part of unmanned aerial vehicle (UAV) swarms task planning and the key technology to improve autonomy. The realization of dynamic task allocation in UAV swarms for ground targets is very difficult because of the large uncertainty of swarms, the target and environment state, and the high real-time allocation requirements. Hence, dynamic task allocation of UAV swarms oriented to ground targets has become a key and difficult problem in the field of mission planning. In this work, a dynamic task allocation method for UAV swarms oriented to ground targets is comprehensively and systematically summarized from two aspects: the establishment of an allocation model and the solution of the allocation model. First, the basic concept and trigger scenario are introduced. Second, the research status and the advantages and disadvantages of the two allocation models are analyzed. Third, the research status and the advantages and disadvantages of several common dynamic task allocation algorithms, such as the algorithm based on market mechanisms, intelligent optimization algorithm, and clustering algorithm, are evaluated. Finally, the specific problems of the current UAV swarm dynamic task allocation method for ground targets are highlighted, and future research directions are established. This work offers important reference significance for fully understanding the current situation of UAV swarm dynamic task allocation technology.
- Published
- 2021
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6. Target Signatures and Pose Estimation
- Author
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Hodžić, Migdat I., Namas, Tarik, Kacprzyk, Janusz, Series Editor, Gomide, Fernando, Advisory Editor, Kaynak, Okyay, Advisory Editor, Liu, Derong, Advisory Editor, Pedrycz, Witold, Advisory Editor, Polycarpou, Marios M., Advisory Editor, Rudas, Imre J., Advisory Editor, Wang, Jun, Advisory Editor, Hadžikadić, Mirsad, editor, and Avdaković, Samir, editor
- Published
- 2017
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7. Optimal Multi-Target Overflight Using Ground-Track Adjustment.
- Author
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Mok, Sung-Hoon and Bang, Hyochoong
- Subjects
ANALYTICAL solutions ,ARTIFICIAL satellite tracking ,SPACE trajectories ,MAXIMA & minima - Abstract
This study proposes a near-optimal, impulsive control method for overflying ground targets. A set of impulses, which adjusts the satellite ground trajectory to enable the overflight, is derived. The proposed impulsive solution is expressed in closed-form which only consists of orbital revolution numbers and target overflight errors. It allows not only simplifying the search for a minimum delta-v solution but also facilitating its extension to the multiple-target overflight problem. It is also provided in this paper an insight connecting the overflight problem to a relative orbit transfer problem controlling a phase angle or mean anomaly. Numerical examples for single-, two-, and three-target overflight verify that the controlled trajectory with the proposed impulsive solution successfully overflies the designated targets within a prescribed time. It is also demonstrated that the total delta-v required for the proposed method is near-optimal based on the performance comparison with a numerical optimization-based method which employs a very large set of initial guesses. [ABSTRACT FROM AUTHOR]
- Published
- 2021
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- View/download PDF
8. Range‐only control for cooperative target circumnavigation of unmanned aerial vehicles.
- Author
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Zhang, Min, Lin, Yun, Hao, Huixin, and Mei, Jingsong
- Subjects
VOYAGES around the world ,DRONE aircraft ,COOPERATION ,GLOBAL Positioning System ,LIPSCHITZ spaces - Abstract
This article deals with cooperative target circumnavigation control strategy for a team of unmanned aerial vehicles (UAVs) when only range measurements are available. First, we propose novel guidance laws based solely on range measurements for tracking and cooperation. Then, convergence and stability of the proposed guidance laws are proved by a rigorous inference of mathematics. Moreover, an illustrative simulation shows that the controlled UAVs orbit around a target and maintain even spacing along the common circle, which confirms the performance of the proposed guidance algorithms. [ABSTRACT FROM AUTHOR]
- Published
- 2020
- Full Text
- View/download PDF
9. Improved 2D Ground Target Tracking in GPS-Based Passive Radar Scenarios
- Author
-
Pedro Gomez-del-Hoyo, Nerea del-Rey-Maestre, María-Pilar Jarabo-Amores, David Mata-Moya, and María-de-Cortés Benito-Ortiz
- Subjects
passive radar ,GPS ,array ,ground target ,GNSS ,Chemical technology ,TP1-1185 - Abstract
Global Positioning System (GPS) satellites offer promising opportunity for Passive Radar systems due to their global coverage and the availability of multiple satellites throughout the world. However, their low power at ground level limits system coverage. In this paper, a GPS based Passive Radar which exploits a single illumination source, and uses digital array processing for ground targets localization is presented. To face signal power problems, a processing scheme combining reconstructed reference signals, adaptive filtering techniques and spatial filtering is implemented. Conventional beamforming techniques are used to increase the level of the target echo before the detection stage, and high resolution DoA estimation techniques are applied to estimate targets azimuth. Ground target localization in local Cartesian space is performed taking into account the system geometry, range and azimuth information. Both synthetic and real radar data are used to analyse system operation. During the measurement campaign, a cooperative vehicle was used for validation purposes. Results confirm that ground targets detection and localization are feasible using a single GPS transmitter.
- Published
- 2022
- Full Text
- View/download PDF
10. Просторово-спектральні методи підвищення ефективності артилерійської розвідки
- Subjects
наземна ціль ,reconnaissance and fire system ,цикл спостереження ,model experiment ,detection ,observation cycle ,модельний експеримент ,виявлення ,інформативність багатоспектрального моніторингу ,nformation content of multispectral monitoring ,розвідувально-вогнева система ,ground target - Abstract
The author analyzes the evolution of reconnaissance-fire technology based on reconnaissance-strike (RSS) and reconnaissance-fire (RFS) systems and its transition to the ideology of reconnaissance-fire systems (RFS). Based on Boyd's cybernetic model, the situational model of RFS combat control and the issue of optimizing it in terms of the "observe" cycle are considered. Practical ways of implementing the developed approach based on multichannel spatial and multispectral processing of intelligence information are substantiated. The optimality of the developed approach is confirmed by the results of a model experiment. A methodology for adapting the characteristics of multi-channel processing of location information to a dynamically changing mobile phone environment has been developed. The optimality of the developed approach is confirmed by the results of the model experiment, and the practical feasibility is confirmed by the patent for the invention.The maximum combat effectiveness of the first stage of the Boyd cycle (artillery reconnaissance) – range, accuracy, target channel, immunity - is achieved by the integration of ground-based radar means of reconnaissance of firing positions and UAVs with multispectral surveillance equipment. The practical significance of the obtained results is provided by the independence of targeting accuracy from the target range with simultaneous provision of round-the-clock operation, all-weather operation, interference resistance and potential informativeness of artillery reconnaissance. The attainable gain in artillery reconnaissance effectiveness indicators is 7.2 times the range, and 20 times the target channel. All analytical results are aimed at implementation in the practice of designing the production of equipment for ground and on-board reconnaissance components., Виконано аналіз еволюції розвідувально-вогневої технології на основі розвідувально-ударних (РУК) і розвідувально-вогневих (РВК) комплексів і переходу її в ідеологію розвідувально-вогневих систем (РВС). На основі кібернетичної моделі Бойда оптимізовано цикл “observe(спостерігай)”. Обґрунтовані практичні шляхи реалізації розробленого підходу на основі багатоканальної просторової і багатоспектральної обробки розвідувальної інформації. Розроблена методологія адаптації характеристик багатоканальної обробки локаційної інформації під цілефонову обстановку, яка динамічно міняється. Оптимальність розробленого підходу підтверджена результатами модельного експерименту, а практична реалізуємість – патентом на винахід. Практична значимість отриманих результатів забезпечується незалежністю точності цілевказання від дальності цілі з одночасним забезпеченням цілодобовості, всепогодності, завадостійкості і потенційної інформативності артилерійської розвідки. Досягаємий виграш в показниках ефективності артилерійської розвідки складає за дальністю – 7,2 рази, за цільовою канальністю–20 раз. Всі аналітичні результати орієнтовані на впровадження в практику проектування виробництва апаратури наземної і бортової компонент розвідки.
- Published
- 2023
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11. Concealed Target Detection with Fusion of Visible and Infrared
- Author
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Saponaro, Philip, Sherbondy, Kelly, Kambhamettu, Chandra, Hutchison, David, Series editor, Kanade, Takeo, Series editor, Kittler, Josef, Series editor, Kleinberg, Jon M., Series editor, Kobsa, Alfred, Series editor, Mattern, Friedemann, Series editor, Mitchell, John C., Series editor, Naor, Moni, Series editor, Nierstrasz, Oscar, Series editor, Pandu Rangan, C., Series editor, Steffen, Bernhard, Series editor, Terzopoulos, Demetri, Series editor, Tygar, Doug, Series editor, Weikum, Gerhard, Series editor, Bebis, George, editor, Boyle, Richard, editor, Parvin, Bahram, editor, Koracin, Darko, editor, McMahan, Ryan, editor, Jerald, Jason, editor, Zhang, Hui, editor, Drucker, Steven M., editor, Kambhamettu, Chandra, editor, El Choubassi, Maha, editor, Deng, Zhigang, editor, and Carlson, Mark, editor
- Published
- 2014
- Full Text
- View/download PDF
12. μ-UAV Based Dynamic Target Tracking for Surveillance and Exploration
- Author
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Bhaskar, Harish, Dias, Jorge, Seneviratne, Lakmal, Al-Mualla, Mohammed, Hutchison, David, Series editor, Kanade, Takeo, Series editor, Kittler, Josef, Series editor, Kleinberg, Jon M., Series editor, Kobsa, Alfred, Series editor, Mattern, Friedemann, Series editor, Mitchell, John C., Series editor, Naor, Moni, Series editor, Nierstrasz, Oscar, Series editor, Pandu Rangan, C., Series editor, Steffen, Bernhard, Series editor, Terzopoulos, Demetri, Series editor, Tygar, Doug, Series editor, Weikum, Gerhard, Series editor, Bebis, George, editor, Boyle, Richard, editor, Parvin, Bahram, editor, Koracin, Darko, editor, McMahan, Ryan, editor, Jerald, Jason, editor, Zhang, Hui, editor, Drucker, Steven M., editor, Kambhamettu, Chandra, editor, El Choubassi, Maha, editor, Deng, Zhigang, editor, and Carlson, Mark, editor
- Published
- 2014
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13. New Low-Cost Video Camera Pointing Mechanism for Stratospheric Balloons: Design and Operational Tests
- Author
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Jaworski, Jarosław, Bobrowski, Kamil, Boruc, Łukasz, Gedroyć, Krzysztof, Macioszek, Krystyna, Rybus, Tomasz, and Sąsiadek, Jerzy, editor
- Published
- 2013
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14. Gyroscopic Control in Self-Guidance Systems of Flying Objects
- Author
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Awrejcewicz, Jan, Koruba, Zbigniew, Awrejcewicz, Jan, and Koruba, Zbigniew
- Published
- 2012
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15. A unitized guidance law for over-flight and standoff tracking of a ground target with fixed wing unmanned aerial vehicle.
- Author
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Zhang, Min, Xia, Weizheng, and Chen, Xin
- Subjects
DRONE aircraft ,TRACKING control systems ,LYAPUNOV functions - Abstract
Over-flight and standoff tracking are the two typical modes of fixed wing unmanned aerial vehicle tracking ground targets. The guidance law of each mode is usually designed independently and thus shows different forms. In this paper, based on the constraints on unmanned aerial vehicle flight, a novel unitized guidance law, which is compatible with these two modes, is proposed. The stability of the guidance law is rigorously proved by a Lyapunov function, and the design of guidance parameters is discussed. Numerical simulation results show that the proposed guidance law can be used for automatically tracking the stationary and moving ground targets well, and also can switch between the two tracking modes smoothly. [ABSTRACT FROM AUTHOR]
- Published
- 2018
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16. Autonomous Target Detection and Localization Using Cooperative Unmanned Aerial Vehicles
- Author
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Yoon, Youngrock, Gruber, Scott, Krakow, Lucas, Pack, Daniel, Morari, Manfred, editor, Thoma, Manfred, editor, Hirsch, Michael J., editor, Commander, Clayton W., editor, Pardalos, Panos M., editor, and Murphey, Robert, editor
- Published
- 2009
- Full Text
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17. Fixed-wing UAV guidance law for ground target over-flight tracking.
- Author
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ZHANG Min, ZHENG Chenming, and HUANG Kun
- Subjects
- *
DRONE aircraft , *ACCELERATION (Mechanics) , *LYAPUNOV functions , *COMPUTER simulation , *STABILITY (Mechanics) - Abstract
This paper studies the problem of tracking a ground target for a fixed-wing unmanned aerial vehicle (UAV) based on the proposed guidance law. The algorithm ensures that a UAV continuously overflies the target whether it is fixed or moving. The requirements of the UAV flight constraints such as bounded air-speed and acceleration are considered. A Lyapunov function is constructed to prove the stability of the proposed guidance law, and parameter design criteria have been developed. Considering the fixed and moving ground targets, numerical simulations are performed to verify the feasibility and benefits of the proposed guidance algorithm. [ABSTRACT FROM AUTHOR]
- Published
- 2019
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18. Simultaneous Localization and Planning for Cooperative Air Munitions
- Author
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Sinclair, Andrew J., Prazenica, Richard J., Jeffcoat, David E., Morari, Manfred, editor, Thoma, Manfred, editor, Pardalos, Panos M., editor, Murphey, Robert, editor, Grundel, Don, editor, and Hirsch, Michael J., editor
- Published
- 2007
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19. BioCaMPS - Support Activities on E2E Calibration and Mission Performance Aspects: External Calibration Transponder Report Issue 4
- Author
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Weidenhaupt, Klaus Frank, Schwerdt, Marco, and Klenk, Patrick
- Subjects
Ground Target ,Overall SAR System Calibration ,External Calibration ,Calibration ,BioCaMPS ,Biomass Calibration Transponder ,P-Band SAR ,Biomass ,Biomass mission ,Active SAR Calibrators ,Calibration Targets ,Transponder - Published
- 2022
20. Unmanned aerial vehicle guidance law for ground target circumnavigation using range-based measurements.
- Author
-
Zhang, Min, Tian, Pengfei, and Chen, Xin
- Abstract
In this paper, a new guidance law using range-based measurements is proposed. Firstly, the new guidance law is designed for circumnavigating a ground target using range and range-rate measurements; Secondly, a Lyapunov function is designed to prove the stability of the proposed guidance law. Compared with the existing ones, this guidance law is more compact. Simulation results show that the guidance law can achieve the circumnavigating task well for the stationary ground target. [ABSTRACT FROM AUTHOR]
- Published
- 2017
- Full Text
- View/download PDF
21. 지상 접근 표적 감지를 위한 초소형 K-대역 레이다 연구.
- Author
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종수, 노진입, 최재현, 이한진, and 박영식
- Abstract
This paper proposes a compact K-band radar applied to a miniature proximity fuze for the active defense system. In this terrestrial environment, it is not easy to detect approaching small targets because the clutter is scattered. In addition, it is difficult to miniaturize the radar for the small proximity fuze while improving the target accuracy of the radar in such environments. To solve these difficulties, this study presents system analysis and design, antenna design, and transceiver and signal processor design of the compact K-band radar. Some test results are presented and the results are analyzed, the validity of the proposed study is examined. [ABSTRACT FROM AUTHOR]
- Published
- 2017
- Full Text
- View/download PDF
22. Improved 2D Ground Target Tracking in GPS-Based Passive Radar Scenarios
- Author
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David Mata-Moya, María de Cortes Benito Ortiz, Pedro José Gómez del Hoyo, María Pilar Jarabo Amores, and Nerea Del Rey
- Subjects
passive radar ,GPS ,array ,ground target ,GNSS ,Electrical and Electronic Engineering ,Biochemistry ,Instrumentation ,Atomic and Molecular Physics, and Optics ,Analytical Chemistry - Abstract
Global Positioning System (GPS) satellites offer promising opportunity for Passive Radar systems due to their global coverage and the availability of multiple satellites throughout the world. However, their low power at ground level limits system coverage. In this paper, a GPS based Passive Radar which exploits a single illumination source, and uses digital array processing for ground targets localization is presented. To face signal power problems, a processing scheme combining reconstructed reference signals, adaptive filtering techniques and spatial filtering is implemented. Conventional beamforming techniques are used to increase the level of the target echo before the detection stage, and high resolution DoA estimation techniques are applied to estimate targets azimuth. Ground target localization in local Cartesian space is performed taking into account the system geometry, range and azimuth information. Both synthetic and real radar data are used to analyse system operation. During the measurement campaign, a cooperative vehicle was used for validation purposes. Results confirm that ground targets detection and localization are feasible using a single GPS transmitter.
- Published
- 2022
- Full Text
- View/download PDF
23. BioCaMPS - Support Activities on E2E Calibration and Mission Performance Aspects: External Calibration Transponder Report Issue 3
- Author
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Weidenhaupt, Klaus Frank, Schwerdt, Marco, and Klenk, Patrick
- Subjects
Ground Target ,Overall SAR System Calibration ,External Calibration ,Calibration ,BioCaMPS ,Biomass Calibration Transponder ,P-Band SAR ,Biomass ,Biomass mission ,Active SAR Calibrators ,Calibration Targets ,Transponder - Published
- 2022
24. Dismantlement and Destruction of Conventional Weapons
- Author
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Pöhlmann, Jürgen and Schulte, Nancy Turtle, editor
- Published
- 1997
- Full Text
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25. The Effect of Seasonal Factors on Geological Interpretation of MSS Data
- Author
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Yuan, D., Robinson, J. E., Duggin, M. J., Merriam, Daniel F., and Förster, Andrea
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- 1996
- Full Text
- View/download PDF
26. BioCaMPS - Support Activities on E2E Calibration and Mission Performance Aspects: External Calibration Transponder Report Issue 2
- Author
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Weidenhaupt, Klaus Frank, Schwerdt, Marco, and Klenk, Patrick
- Subjects
Ground Target ,Overall SAR System Calibration ,External Calibration ,Calibration ,BioCaMPS ,Biomass Calibration Transponder ,P-Band SAR ,Biomass ,Biomass mission ,Active SAR Calibrators ,Calibration Targets ,Transponder - Published
- 2021
27. Orbit design for hybrid ground-space targets.
- Author
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Zhang, Haiyang, Zhang, Gang, and Tian, Longfei
- Subjects
- *
ORBITS (Astronomy) , *NONLINEAR equations , *PROBLEM solving - Abstract
For operationally responsive space missions, traditional orbit design problems are only for a single type of targets, i.e., only ground targets or only space targets. This paper studies the hybrid ground and space targets of interest by considering J 2 perturbation. The ground-target visit problem needs the ground track of the designed orbit to pass through the ground target, and one ground target corresponds to one equality constraint. The space-target visit problem is viewed as the orbit flyby problem, and one space target corresponds to two equality constraints. According to the numbers of designed variables and equality constraints, there are two cases for the maximum number of hybrid targets: (1) two ground targets and two space targets; (2) four ground targets and one space target. For given orbital inclination and right ascension of ascending node, the other orbital elements of the designed orbit are obtained by numerical methods. Then, the problem is transformed into solving nonlinear equations only of two variables. Newton-Raphson iterations are adopted to solve the problem, and the initial guesses are obtained by the grid search method. Several numerical examples are presented to validate the proposed orbit design approach for hybrid ground-space targets. [ABSTRACT FROM AUTHOR]
- Published
- 2022
- Full Text
- View/download PDF
28. BioCaMPS - Support Activities on E2E Calibration and Mission Performance Aspects: External Calibration Transponder Report Issue 1
- Author
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Weidenhaupt, Klaus Frank, Schwerdt, Marco, and Klenk, Patrick
- Subjects
Ground Target ,Overall SAR System Calibration ,External Calibration ,Calibration ,BioCaMPS ,Biomass Calibration Transponder ,P-Band SAR ,Biomass ,Biomass mission ,Active SAR Calibrators ,Calibration Targets ,Transponder - Published
- 2020
29. Improved 2D Ground Target Tracking in GPS-Based Passive Radar Scenarios.
- Author
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Gomez-del-Hoyo, Pedro, del-Rey-Maestre, Nerea, Jarabo-Amores, María-Pilar, Mata-Moya, David, and Benito-Ortiz, María-de-Cortés
- Subjects
- *
PASSIVE radar , *BISTATIC radar , *GLOBAL Positioning System , *ARRAY processing , *SPATIAL filters , *ADAPTIVE filters - Abstract
Global Positioning System (GPS) satellites offer promising opportunity for Passive Radar systems due to their global coverage and the availability of multiple satellites throughout the world. However, their low power at ground level limits system coverage. In this paper, a GPS based Passive Radar which exploits a single illumination source, and uses digital array processing for ground targets localization is presented. To face signal power problems, a processing scheme combining reconstructed reference signals, adaptive filtering techniques and spatial filtering is implemented. Conventional beamforming techniques are used to increase the level of the target echo before the detection stage, and high resolution DoA estimation techniques are applied to estimate targets azimuth. Ground target localization in local Cartesian space is performed taking into account the system geometry, range and azimuth information. Both synthetic and real radar data are used to analyse system operation. During the measurement campaign, a cooperative vehicle was used for validation purposes. Results confirm that ground targets detection and localization are feasible using a single GPS transmitter. [ABSTRACT FROM AUTHOR]
- Published
- 2022
- Full Text
- View/download PDF
30. Automatic Target Recognition of SAR Images Based on Global Scattering Center Model.
- Author
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Jianxiong, Zhou, Zhiguang, Shi, Xiao, Cheng, and Qiang, Fu
- Subjects
- *
SYNTHETIC aperture radar , *AUTOMATION , *IMAGING systems , *SCATTERING (Physics) , *FEATURE extraction , *PREDICTION models , *ELECTROMAGNETISM - Abstract
This paper proposes a synthetic aperture radar (SAR) automatic target recognition approach based on a global scattering center model. The scattering center model is established offline using range profiles at multiple viewing angles, so the original data amount is much less than that required for establishing SAR image templates. Scattering center features at different target poses can be conveniently predicted by this model. Moreover, the model can be modified to predict features for various target configurations. For the SAR image to be classified, regional features in different levels are extracted by thresholding and morphological operations. The regional features will be matched to the predicted scattering center features of different targets to arrive at a decision. This region-to-point matching is much easier to implement and is less sensitive to nonideal factors such as noise and pose estimation error than point-to-point matching. A matching scheme going through from coarse to fine regional features in the inner cycle and going through different pose hypotheses in the outer cycle is designed to improve the efficiency and robustness of the classifier. Experiments using both data predicted by a high-frequency electromagnetic (EM) code and data measured in the MSTAR program verify the validity of the method. [ABSTRACT FROM AUTHOR]
- Published
- 2011
- Full Text
- View/download PDF
31. Space-Strike Arms and International Security
- Author
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Sagdeev, Roald, Kokoshin, Andrei, Holdren, John, editor, and Rotblat, Joseph, editor
- Published
- 1987
- Full Text
- View/download PDF
32. Smart Weapons: Trends and Capabilities
- Author
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Newbery, A. R. and Boyd-Carpenter, Thomas
- Published
- 1989
- Full Text
- View/download PDF
33. Experimental operation of drone micro‐SAR with efficient time‐varying velocity compensation.
- Author
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Lee, W.K. and Lee, K.W.
- Abstract
Drone platform for synthetic aperture radar (SAR) operation has been little publicised due to the technical constraint of the payload implementation. Multi‐rotor drone based SAR is distinguished from the conventional airborne system by the increased sensitivity to turbulences and poor motion stability. Extremely limited power and mass budgets may prevent the use of extra hardware for motion compensation and the difficulty of SAR focusing is aggravated. Feasibility of micro‐SAR drone operation is investigated through field tests, where experimental SAR images are acquired over ground targets. Attempts have been made to implement near‐real‐time compensation for non‐uniform motion disturbance. Finally, experimental drone SAR operation is validated through calibrated SAR images. [ABSTRACT FROM AUTHOR]
- Published
- 2017
- Full Text
- View/download PDF
34. Unified fast numerical algorithm for calculation of EM field of dipole located at arbitrary distance from the boundary of dielectric media
- Author
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Oleg I. Sukharevsky and G. S. Zalevsky
- Subjects
Electromagnetic field ,Physics ,Dipole ,Transition dipole moment ,Discrete dipole approximation codes ,Boundary (topology) ,Computational electromagnetics ,Discrete dipole approximation ,dipole ,ground target ,integral equation ,low-altitude target ,scattering characteristics ,Integral equation ,Algorithm - Abstract
An algorithm is considered for calculating the EM field of dipole in case of arbitrary spacing between the point of dipole location and the point of its field observation, as well as arbitrary distance of points from the boundary of dielectric half-spaces. The algorithm is adapted to the height of mentioned points above the boundary and allows to reduce significantly calculation time while providing given accuracy of the dipole EM field component calculation. Results of calculation of radar scattering characteristics are demonstrated for low-altitude and ground objects obtained using the developed calculation technique based on integral equation solution, and using proposed algorithm for dipole EM field calculation.
- Published
- 2015
35. Савремене методе употребе летелица нове генерације при дејству на покретне циљеве у ваздуху и на земљи
- Author
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Pekić, Nikola Đ., Stupar, Slobodan, Petrović, Zlatko, Kostić, Ivan, and Gvozdenović, Slobodan
- Subjects
наоружање ,attack manoeuvre ,земаљски циљ ,flight mode ,мод лета ,маневар напада ,engine thrust vector deflection ,boundary layer ,ground target ,simulation mode of aircraft motion ,manoeuvre properties ,симулациони модел кретања авиона ,weaponry ,гранични слој ,отклон вектора потиска мотора ,маневарске карактеристике - Abstract
У овој дисертацији приказан је симулациони модел понашања летелице у прелазним режимима лета, односно модел разматраног система. У симулационом моделу примењен је комплетан модел кретања авиона као крутог тела са шест степени слободе. Примена комплетног модела кретања авиона је важна за прорачун динамике лета летелице и добијања оцене о њеним укупним маневарским карактеристикама. Такође, примена комплетног модела кретања авиона омогућава детерминисање аеродинамичких и инерционих сила које делују на летелицу, као и момената који се јављају на деловима структуре летелице у одређеним режимима лета или при маневрисању и могу се користити при пројектовању структуре летелице. Управљање летелицом је сложен процес и пред пилота поставља бројне захтеве по питању комплексности задатака који се извршавају или које треба да изврши применом што једноставније технике пилотирања као и управљачких алгоритама који су лако применљиви на летелици, с тим да се добије поуздан систем управљања. Због оваквих захтева који су често опречни, проблематика управљања летелицом се још више усложњава, стога се на почетку пројектовања летелице спроводе правовремене анализе динамичких карактеристика система управљања и провере у симулационим условима на земљи (симулатори лета) и у лету на летелицама које су посебно опремљене за овакве намене. У складу са већ реченим, у дисертацији, дата је анализа промена маневарских особина авиона при отклону вектора потиска мотора, као и приказ могућности побољшања вероватноће уништења земаљског циља нападом из обрушавања после борбеног заокрета. При том се кретање летелице посматрало у контексту остварених транслаторних убрзања у уздужном и нормалном правцу. Дата анализа побољшања перформанси лета борбеног авиона односи се на терминалну фазу напада на земаљске циљеве, односно етапу обрушавања, на којој се остварује довођење авиона у почетне потребне услове за остваривање дејства. Анализа побољшања перформанси урађена је за две конфигурације авиона са вертикалним полетањем и слетањем и то: конфигурација са мешовитом погонском групом састављеном од узгонских и маршевских мотора и конфигурација са једним или два векторисана узгонско- потисна мотора. Такође, приказани су резултати симулације перформанси авиона са векторисаним потиском као и напредни модови управљања летом летелице са предлозима мера и поступака за сваку конкретну ситуацију/мод лета... Simulation model of the aircraft conduct in transient flying regimes is shown in this dissertation. A complete motion model of the aircraft as a six degree of freedom rigid body is applied in the simulation model. Application of complete aircraft motion model is important for the aircraft flight dynamics computation and getting the evaluation of its complete manoeuvrability as well. Also, the application of a complete aircraft motion model provides determination of aerodynamic and inertial forces which affect the aircraft, as well as the moments which appear at the aircraft structure parts during the specific flight regimes or during manoeuvring and can be used in aircraft structure (frame) design. Aircraft control is a complex process and posts many demands in front of a pilot concerning complexity of the task being done or which should be done by applying the simplest technique of piloting, as well as control algorithms easy to be applied on the aircraft, with the goal of achieving reliable control system. Due to these demands which are often opposite, the issue of aircraft control is getting more complex, and that’s why at the beginning of the aircraft designing process we conduct forehand analyses of control system dynamic characteristics and tests in simulated conditions on the ground (flight simulators) and in the flight on the aircraft specially equipped for these purposes. According to the mentioned above, in this dissertation, the analysis of aircraft maneuvering characteristics transitions during the engine thrust vector deflection is specified, as well as the preview of the opportunities for improving probability of the destruction of a ground target in the course of diving after combat turn. In this, the aircraft motion has been considered in the context of performed translatory accelerations in longitudinal and perpendicular direction. The given analyses on the improvement of the combat aircraft flight performances refers to the terminal phase of the attack on the ground targets, that is, a diving phase, in which the aircraft is placed in the initial necessary conditions for the action accomplishment. The analyses of the performances improvement has been carried out for two types of VTOL aircraft configurations, namely: the configuration with mixed power group, consisting of lift and march engines and the configuration with single or twin thrustlifted engines. Also, the simulation results of vector thrust aircraft performances are shown, as well as the advanced flight aircraft control modes with proposals of the measures and procedures for each specific situation/flight mode...
- Published
- 2013
36. Савремене методе употребе летелица нове генерације при дејству на покретне циљеве у ваздуху и на земљи
- Author
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Stupar, Slobodan, Petrović, Zlatko, Kostić, Ivan, Gvozdenović, Slobodan, Pekić, Nikola Đ., Stupar, Slobodan, Petrović, Zlatko, Kostić, Ivan, Gvozdenović, Slobodan, and Pekić, Nikola Đ.
- Abstract
У овој дисертацији приказан је симулациони модел понашања летелице у прелазним режимима лета, односно модел разматраног система. У симулационом моделу примењен је комплетан модел кретања авиона као крутог тела са шест степени слободе. Примена комплетног модела кретања авиона је важна за прорачун динамике лета летелице и добијања оцене о њеним укупним маневарским карактеристикама. Такође, примена комплетног модела кретања авиона омогућава детерминисање аеродинамичких и инерционих сила које делују на летелицу, као и момената који се јављају на деловима структуре летелице у одређеним режимима лета или при маневрисању и могу се користити при пројектовању структуре летелице. Управљање летелицом је сложен процес и пред пилота поставља бројне захтеве по питању комплексности задатака који се извршавају или које треба да изврши применом што једноставније технике пилотирања као и управљачких алгоритама који су лако применљиви на летелици, с тим да се добије поуздан систем управљања. Због оваквих захтева који су често опречни, проблематика управљања летелицом се још више усложњава, стога се на почетку пројектовања летелице спроводе правовремене анализе динамичких карактеристика система управљања и провере у симулационим условима на земљи (симулатори лета) и у лету на летелицама које су посебно опремљене за овакве намене. У складу са већ реченим, у дисертацији, дата је анализа промена маневарских особина авиона при отклону вектора потиска мотора, као и приказ могућности побољшања вероватноће уништења земаљског циља нападом из обрушавања после борбеног заокрета. При том се кретање летелице посматрало у контексту остварених транслаторних убрзања у уздужном и нормалном правцу. Дата анализа побољшања перформанси лета борбеног авиона односи се на терминалну фазу напада на земаљске циљеве, односно етапу обрушавања, на којој се остварује довођење авиона у почетне потребне услове за остваривање дејства. Анализа побољшања перформанси урађена је за две конфигурације авиона са вертикалним, Simulation model of the aircraft conduct in transient flying regimes is shown in this dissertation. A complete motion model of the aircraft as a six degree of freedom rigid body is applied in the simulation model. Application of complete aircraft motion model is important for the aircraft flight dynamics computation and getting the evaluation of its complete manoeuvrability as well. Also, the application of a complete aircraft motion model provides determination of aerodynamic and inertial forces which affect the aircraft, as well as the moments which appear at the aircraft structure parts during the specific flight regimes or during manoeuvring and can be used in aircraft structure (frame) design. Aircraft control is a complex process and posts many demands in front of a pilot concerning complexity of the task being done or which should be done by applying the simplest technique of piloting, as well as control algorithms easy to be applied on the aircraft, with the goal of achieving reliable control system. Due to these demands which are often opposite, the issue of aircraft control is getting more complex, and that’s why at the beginning of the aircraft designing process we conduct forehand analyses of control system dynamic characteristics and tests in simulated conditions on the ground (flight simulators) and in the flight on the aircraft specially equipped for these purposes. According to the mentioned above, in this dissertation, the analysis of aircraft maneuvering characteristics transitions during the engine thrust vector deflection is specified, as well as the preview of the opportunities for improving probability of the destruction of a ground target in the course of diving after combat turn. In this, the aircraft motion has been considered in the context of performed translatory accelerations in longitudinal and perpendicular direction. The given analyses on the improvement of the combat aircraft flight performances refers to the terminal phase of the at
- Published
- 2013
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